Dr. Pletser’s experience includes 30 years of working with the European Space Agency as a Senior Physicist/Engineer and coordinating their parabolic flight campaigns, and he is the Guinness World Record holder for the most number of aircraft flown (12) in parabolas, personally logging more than 7,300 parabolas.
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Seeing the 5,000th book published makes us at the same time proud, happy, humble, and grateful. This is a great opportunity to stop and celebrate what we have done so far, but is also an opportunity to engage even more, grow, and succeed. It wouldn't be possible to get here without the synergy of team members’ hard work and authors and editors who devote time and their expertise into Open Access book publishing with us.
\\n\\n
Over these years, we have gone from pioneering the scientific Open Access book publishing field to being the world’s largest Open Access book publisher. Nonetheless, our vision has remained the same: to meet the challenges of making relevant knowledge available to the worldwide community under the Open Access model.
\\n\\n
We are excited about the present, and we look forward to sharing many more successes in the future.
\\n\\n
Thank you all for being part of the journey. 5,000 times thank you!
\\n\\n
Now with 5,000 titles available Open Access, which one will you read next?
Preparation of Space Experiments edited by international leading expert Dr. Vladimir Pletser, Director of Space Training Operations at Blue Abyss is the 5,000th Open Access book published by IntechOpen and our milestone publication!
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"This book presents some of the current trends in space microgravity research. The eleven chapters introduce various facets of space research in physical sciences, human physiology and technology developed using the microgravity environment not only to improve our fundamental understanding in these domains but also to adapt this new knowledge for application on earth." says the editor. Listen what else Dr. Pletser has to say...
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Dr. Pletser’s experience includes 30 years of working with the European Space Agency as a Senior Physicist/Engineer and coordinating their parabolic flight campaigns, and he is the Guinness World Record holder for the most number of aircraft flown (12) in parabolas, personally logging more than 7,300 parabolas.
\n\n
Seeing the 5,000th book published makes us at the same time proud, happy, humble, and grateful. This is a great opportunity to stop and celebrate what we have done so far, but is also an opportunity to engage even more, grow, and succeed. It wouldn't be possible to get here without the synergy of team members’ hard work and authors and editors who devote time and their expertise into Open Access book publishing with us.
\n\n
Over these years, we have gone from pioneering the scientific Open Access book publishing field to being the world’s largest Open Access book publisher. Nonetheless, our vision has remained the same: to meet the challenges of making relevant knowledge available to the worldwide community under the Open Access model.
\n\n
We are excited about the present, and we look forward to sharing many more successes in the future.
\n\n
Thank you all for being part of the journey. 5,000 times thank you!
\n\n
Now with 5,000 titles available Open Access, which one will you read next?
\n'}],latestNews:[{slug:"webinar-introduction-to-open-science-wednesday-18-may-1-pm-cest-20220518",title:"Webinar: Introduction to Open Science | Wednesday 18 May, 1 PM CEST"},{slug:"step-in-the-right-direction-intechopen-launches-a-portfolio-of-open-science-journals-20220414",title:"Step in the Right Direction: IntechOpen Launches a Portfolio of Open Science Journals"},{slug:"let-s-meet-at-london-book-fair-5-7-april-2022-olympia-london-20220321",title:"Let’s meet at London Book Fair, 5-7 April 2022, Olympia London"},{slug:"50-books-published-as-part-of-intechopen-and-knowledge-unlatched-ku-collaboration-20220316",title:"50 Books published as part of IntechOpen and Knowledge Unlatched (KU) Collaboration"},{slug:"intechopen-joins-the-united-nations-sustainable-development-goals-publishers-compact-20221702",title:"IntechOpen joins the United Nations Sustainable Development Goals Publishers Compact"},{slug:"intechopen-signs-exclusive-representation-agreement-with-lsr-libros-servicios-y-representaciones-s-a-de-c-v-20211123",title:"IntechOpen Signs Exclusive Representation Agreement with LSR Libros Servicios y Representaciones S.A. de C.V"},{slug:"intechopen-expands-partnership-with-research4life-20211110",title:"IntechOpen Expands Partnership with Research4Life"},{slug:"introducing-intechopen-book-series-a-new-publishing-format-for-oa-books-20210915",title:"Introducing IntechOpen Book Series - A New Publishing Format for OA Books"}]},book:{item:{type:"book",id:"10921",leadTitle:null,fullTitle:"Plasma Science and Technology",title:"Plasma Science and Technology",subtitle:null,reviewType:"peer-reviewed",abstract:"Plasma science and technology (PST) is a discipline investigating fundamental transport behaviors, interaction physics, and reaction chemistry of plasma and its applications in different technologies and fields. Plasma has uses in refrigeration, biotechnology, health care, microelectronics and semiconductors, nanotechnology, space and environmental sciences, and so on. This book provides a comprehensive overview of PST, including information on different types of plasma, basic interactions of plasma with organic materials, plasma-based energy devices, low-temperature plasma for complex systems, and much more.",isbn:"978-1-83969-624-4",printIsbn:"978-1-83969-623-7",pdfIsbn:"978-1-83969-625-1",doi:"10.5772/intechopen.95256",price:119,priceEur:129,priceUsd:155,slug:"plasma-science-and-technology",numberOfPages:246,isOpenForSubmission:!1,isInWos:null,isInBkci:!1,hash:"c45670ef4b081fd9eebaf911b2b4627b",bookSignature:"Aamir Shahzad",publishedDate:"February 23rd 2022",coverURL:"https://cdn.intechopen.com/books/images_new/10921.jpg",numberOfDownloads:1383,numberOfWosCitations:0,numberOfCrossrefCitations:0,numberOfCrossrefCitationsByBook:0,numberOfDimensionsCitations:0,numberOfDimensionsCitationsByBook:0,hasAltmetrics:1,numberOfTotalCitations:0,isAvailableForWebshopOrdering:!0,dateEndFirstStepPublish:"March 2nd 2021",dateEndSecondStepPublish:"March 30th 2021",dateEndThirdStepPublish:"May 29th 2021",dateEndFourthStepPublish:"August 17th 2021",dateEndFifthStepPublish:"October 16th 2021",currentStepOfPublishingProcess:5,indexedIn:"1,2,3,4,5,6,7",editedByType:"Edited by",kuFlag:!1,featuredMarkup:null,editors:[{id:"288354",title:"Dr.",name:"Aamir",middleName:null,surname:"Shahzad",slug:"aamir-shahzad",fullName:"Aamir Shahzad",profilePictureURL:"https://mts.intechopen.com/storage/users/288354/images/system/288354.jpg",biography:"Aamir Shahzad has more than seventeen years of experience in university research and teaching both at home and abroad. He received his doctoral and postdoctoral degrees from Xi’an Jiaotong University (XJTU), China, in 2012 and 2015, respectively. His research interests include computational physics, complex fluids/plasmas, CFD, complex Fluids. Currently, Dr. Shahzad is an associate professor in the Department of Physics, the Government College University Faisalabad (GCUF), Pakistan. He is also a member of the ThermoPhysical Society of XJTU, GCUF Physics Society, and the University of Agriculture Faisalabad (UAF), Pakistan.",institutionString:"Government College University Faisalabad",position:null,outsideEditionCount:0,totalCites:0,totalAuthoredChapters:"12",totalChapterViews:"0",totalEditedBooks:"5",institution:{name:"Government College University, Faisalabad",institutionURL:null,country:{name:"Pakistan"}}}],equalEditorOne:null,equalEditorTwo:null,equalEditorThree:null,coeditorOne:null,coeditorTwo:null,coeditorThree:null,coeditorFour:null,coeditorFive:null,topics:[{id:"229",title:"Plasma Physics",slug:"plasma-physics"}],chapters:[{id:"77718",title:"Cold Atmospheric Pressure Plasma Technology for Biomedical Application",doi:"10.5772/intechopen.98895",slug:"cold-atmospheric-pressure-plasma-technology-for-biomedical-application",totalDownloads:207,totalCrossrefCites:0,totalDimensionsCites:0,hasAltmetrics:0,abstract:"Cold plasma generated in an open environment with a temperature nearly around room temperature has recently been a topic of great importance. It has unlocked the door of plasma application in a new direction: biomedical applications. Cold atmospheric pressure (CAP) plasma comprises various neutral and charged reactive species, UV radiations, electric current/fields etc., which have several impactful effects on biological matter. Some of the significant biological effects of CAP plasma are inactivation of microorganism, stimulation of cell proliferation and tissue regeneration, destruction of cells by initializing apoptosis etc. Although the detailed mechanism of action of plasma on biomaterials is still not completely understood, some basic principles are known. Studies have indicated that the reactive oxygen species and nitrogen species (ROS, RNS) play a crucial role in the observed biological effects. In this perspective, this chapter first provides a brief discussion on the fundamentals of CAP plasma and its generation methods. Then a discussion on the optical diagnostics methods to characterize the plasma is provided. Optical emission spectroscopy (OES) is used to identify the reactive species and to measure their relative concentration. Other important plasma parameters such as gas temperature, electron/excitation temperature and electron density measurement methods using OES have also been discussed. Then a discussion on the application of CAP plasma in biomedical field is provided. A thorough understanding of biochemical reaction mechanisms involving highly reactive plasma species will further improve and extend CAP plasma technology in biomedical applications.",signatures:"Rakesh Ruchel Khanikar and Heremba Bailung",downloadPdfUrl:"/chapter/pdf-download/77718",previewPdfUrl:"/chapter/pdf-preview/77718",authors:[{id:"355846",title:"Prof.",name:"Heremba",surname:"Bailung",slug:"heremba-bailung",fullName:"Heremba Bailung"},{id:"355847",title:"Mr.",name:"Rakesh Ruchel",surname:"Khanikar",slug:"rakesh-ruchel-khanikar",fullName:"Rakesh Ruchel Khanikar"}],corrections:null},{id:"78718",title:"An Experimental Investigation on the Thermodynamic Characteristics of DBD Plasma Actuations for Aircraft Icing Mitigation",doi:"10.5772/intechopen.100100",slug:"an-experimental-investigation-on-the-thermodynamic-characteristics-of-dbd-plasma-actuations-for-airc",totalDownloads:54,totalCrossrefCites:0,totalDimensionsCites:0,hasAltmetrics:0,abstract:"We report the research progress made in our research efforts to utilize the thermal effects induced by DBD plasma actuation to suppress dynamic ice accretion over the surface of an airfoil/wing model for aircraft icing mitigation. While the fundamental mechanism of thermal energy generation in DBD plasma discharges were introduced briefly, the significant differences in the working mechanisms of the plasma-based surface heating approach from those of conventional resistive electric heating methods were highlighted for aircraft anti−/de-icing applications. By leveraging the unique Icing Research Tunnel available at Iowa State University (i.e., ISU-IRT), a comprehensive experimental campaign was conducted to quantify the thermodynamic characteristics of a DBD plasma actuator exposed to frozen cold incoming airflow coupled with significant convective heat transfer. By embedding a DBD plasma actuator and a conventional electrical film heater on the surface of the same airfoil/wing model, a comprehensive experimental campaign was conducted to provide a side-by-side comparison between the DBD plasma-based approach and conventional resistive electrical heating method in preventing ice accretion over the airfoil surface. The experimental results clearly reveal that, with the same power consumption level, the DBD plasma actuator was found to have a noticeably better performance to suppress ice accretion over the airfoil surface, in comparison to the conventional electrical film heater. A duty-cycle modulation concept was adopted to further enhance the plasma-induced thermal effects for improved anti−/de-icing performance. The findings derived from the present study could be used to explore/optimize design paradigm for the development of novel plasma-based anti−/de-icing strategies tailored specifically for aircraft icing mitigation.",signatures:"Cem Kolbakir, Haiyang Hu, Yang Liu and Hui Hu",downloadPdfUrl:"/chapter/pdf-download/78718",previewPdfUrl:"/chapter/pdf-preview/78718",authors:[{id:"354747",title:"Prof.",name:"Hui",surname:"Hu",slug:"hui-hu",fullName:"Hui Hu"},{id:"427956",title:"Dr.",name:"Cem",surname:"Kolbakir",slug:"cem-kolbakir",fullName:"Cem Kolbakir"},{id:"427957",title:"Dr.",name:"Haiyang",surname:"Hu",slug:"haiyang-hu",fullName:"Haiyang Hu"},{id:"427958",title:"Dr.",name:"Yang",surname:"Liu",slug:"yang-liu",fullName:"Yang Liu"}],corrections:null},{id:"78067",title:"In-Liquid Plasma: A Novel Tool for Nanofabrication",doi:"10.5772/intechopen.98858",slug:"in-liquid-plasma-a-novel-tool-for-nanofabrication",totalDownloads:104,totalCrossrefCites:0,totalDimensionsCites:0,hasAltmetrics:0,abstract:"This chapter focuses on synthesising nanomaterials using an emerging technology called In-Liquid Plasma, i.e., plasma generation inside a liquid. The generation of various reactive species and energetic electrons in the plasma zone plays a crucial role in synthesising nanomaterials. They act as the reducing agent. Non-requirement of the toxic chemical reducing agents make In-Liquid Plasma an environmentally friendly green approach to fabricate nanomaterials. This method enables the simultaneous synthesis of nanoparticles from the electrode material and liquid precursor, which gains much importance on the single-step synthesis of nanocomposites. Moreover, it gives flexibility in controlling both the physical and chemical parameters, which provide fine-tuning required for the size, shape and composition of nanomaterials.",signatures:"Palash Jyoti Boruah, Parismita Kalita and Heremba Bailung",downloadPdfUrl:"/chapter/pdf-download/78067",previewPdfUrl:"/chapter/pdf-preview/78067",authors:[{id:"355846",title:"Prof.",name:"Heremba",surname:"Bailung",slug:"heremba-bailung",fullName:"Heremba Bailung"},{id:"418344",title:"Mr.",name:"Palash",surname:"Jyoti Boruah",slug:"palash-jyoti-boruah",fullName:"Palash Jyoti Boruah"},{id:"420623",title:"Ms.",name:"Parismita",surname:"Kalita",slug:"parismita-kalita",fullName:"Parismita Kalita"}],corrections:null},{id:"79184",title:"Polarized Thermal Conductivity of Two-Dimensional Dusty Plasmas",doi:"10.5772/intechopen.100545",slug:"polarized-thermal-conductivity-of-two-dimensional-dusty-plasmas",totalDownloads:100,totalCrossrefCites:0,totalDimensionsCites:0,hasAltmetrics:0,abstract:"The computation of thermalt properties of dusty plasmas is substantial task in the area of science and technology. The thermal conductivity (λ) has been computed by applying polarization effect through molecular dynamics (MD) simulations of two dimensional (2D) strongly coupled complex dusty plasmas (SCCDPs). The effects of polarization on thermal conductivity have been measured for a wide range of Coulomb coupling (Γ) and Debye screening (κ) parameters using homogeneous non-equilibrium molecular dynamics (HNEMD) method for suitable system sizes. The HNEMD simulation method is employed at constant external force field strength (F*) and varying polarization effects. The algorithm provides precise results with rapid convergence and minute dimension effects. The outcomes have been compared with earlier available simulation results of molecular dynamics, theoretical predictions and experimental results of complex dusty plasma liquids. The calculations show that the kinetic energy of SCCDPS depends upon the system temperature (≡ 1/Г) and it is independent of higher screening parameter. Furthermore, it has shown that the presented HNEMD method has more reliable results than those obtained through earlier known numerical methods.",signatures:"Aamir Shahzad, Madiha Naheed, Aadil Mahboob, Muhammad Kashif, Alina Manzoor and H.E. Maogang",downloadPdfUrl:"/chapter/pdf-download/79184",previewPdfUrl:"/chapter/pdf-preview/79184",authors:[{id:"288354",title:"Dr.",name:"Aamir",surname:"Shahzad",slug:"aamir-shahzad",fullName:"Aamir Shahzad"},{id:"439287",title:"Dr.",name:"Aadil",surname:"Mahboob",slug:"aadil-mahboob",fullName:"Aadil Mahboob"},{id:"439288",title:"Dr.",name:"Muhammad",surname:"Kashif",slug:"muhammad-kashif",fullName:"Muhammad Kashif"},{id:"439289",title:"Dr.",name:"Alina",surname:"Manzoor",slug:"alina-manzoor",fullName:"Alina Manzoor"},{id:"439290",title:"Dr.",name:"H.E.",surname:"Maogang",slug:"h.e.-maogang",fullName:"H.E. Maogang"}],corrections:null},{id:"77814",title:"Studies of Self Diffusion Coefficient in Electrorheological Complex Plasmas through Molecular Dynamics Simulations",doi:"10.5772/intechopen.98854",slug:"studies-of-self-diffusion-coefficient-in-electrorheological-complex-plasmas-through-molecular-dynami",totalDownloads:87,totalCrossrefCites:0,totalDimensionsCites:0,hasAltmetrics:0,abstract:"A molecular dynamics (MD) simulation method has been proposed for three-dimensional (3D) electrorheological complex (dusty) plasmas (ER-CDPs). The velocity autocorrelation function (VACF) and self-diffusion coefficient (D) have been investigated through Green-Kubo expressions by using equilibrium MD simulations. The effect of uniaxial electric field (MT) on the VACF and D of dust particles has been computed along with different combinations of plasma Coulomb coupling (Γ) and Debye screening (κ) parameters. The new simulation results reflect diffusion motion for lower-intermediate to higher plasma coupling (Γ) for the sufficient strength of 0.0 < M ≥ 1.5. The simulation outcomes show that the MT significantly affects VACF and D. It is observed that the strength of MT increases with increasing the Γ and up to κ = 2. Furthermore, it is found that the increasing trend in D for the external applied MT significantly depends on the combination of plasma parameters (Γ, κ). For the lower values of Γ, the proposed method works only for the low strength of MT; at higher Γ, the simulation scheme works for lower to intermediate MT, and D increased almost 160%. The present results are in fair agreement with parts of other MD data in the literature, with our values generally overpredicting the diffusion motion in ER-CDPs. The investigations show that the present algorithm more effective for the liquids-like and solid-like state of ER-CDPs. Thus, current equilibrium MD techniques can be employed to compute the thermophysical properties and also helps to understand the microscopic mechanism in ER-CDPs.",signatures:"Muhammad Asif Shakoori, Maogang He, Aamir Shahzad and Misbah Khan",downloadPdfUrl:"/chapter/pdf-download/77814",previewPdfUrl:"/chapter/pdf-preview/77814",authors:[{id:"191605",title:"Dr.",name:"Aamir",surname:"Shahzad",slug:"aamir-shahzad",fullName:"Aamir Shahzad"},{id:"238571",title:"Prof.",name:"Maogang",surname:"He",slug:"maogang-he",fullName:"Maogang He"},{id:"354349",title:"Ph.D. Student",name:"Muhammad Asif",surname:"Shakoori",slug:"muhammad-asif-shakoori",fullName:"Muhammad Asif Shakoori"},{id:"421284",title:"Ms.",name:"Misbah",surname:"Khan",slug:"misbah-khan",fullName:"Misbah Khan"}],corrections:null},{id:"78438",title:"Transverse Thermal Instability of Radiative Plasma with FLR Corrections for Star Formation in ISM",doi:"10.5772/intechopen.99924",slug:"transverse-thermal-instability-of-radiative-plasma-with-flr-corrections-for-star-formation-in-ism",totalDownloads:93,totalCrossrefCites:0,totalDimensionsCites:0,hasAltmetrics:0,abstract:"Impact of porosity, rotation and finite ion Larmor radius (FLR) corrections on thermal instability of immeasurable homogeneous plasma has been discovered incorporating the effects of radiative heat-loss function and thermal conductivity. The general dispersion relation is carried out with the help of the normal mode analysis scheme taking the suitable linearized perturbation equations of the difficulty. This general dispersion relations is further reduces for rotation axis parallel and perpendicular to the magnetic field. Thermal instability criterion establishes the stability of the medium. Mathematical calculations have been performed to represent the impact of different limitations on the growth rate of thermal instability. It is found that rotation, FLR corrections and medium porosity stabilize the growth rate of the medium in the transverse mode of propagation. Our outcome of the problem explains that the rotation, porosity and FLR corrections affect the dens molecular clouds arrangement and star configuration in interstellar medium.",signatures:"Sachin Kaothekar",downloadPdfUrl:"/chapter/pdf-download/78438",previewPdfUrl:"/chapter/pdf-preview/78438",authors:[{id:"417062",title:"Associate Prof.",name:"Sachin",surname:"Kaothekar",slug:"sachin-kaothekar",fullName:"Sachin Kaothekar"}],corrections:null},{id:"78788",title:"Parametric Interaction of VLF and ELF Waves in the Ionosphere",doi:"10.5772/intechopen.100009",slug:"parametric-interaction-of-vlf-and-elf-waves-in-the-ionosphere",totalDownloads:104,totalCrossrefCites:0,totalDimensionsCites:0,hasAltmetrics:0,abstract:"In this Chapter we analyze a non-linear parametric interaction between Very Low Frequency (VLF) and Extremely Low Frequency (ELF) waves in the ionosphere. We demonstrate that nonlinear parametric coupling between quasi-electrostatic Lower Oblique Resonance (LOR) and ELF waves significantly contributes to the VLF electromagnetic whistler wave spectrum. Analytical and numerical results are compared with experimental data obtained during active space experiments and satellite data. These data clearly show that presence of VLF waves in the region of plasmasphere boundary layer, where there are no injected due to substorm/storm activity energetic electrons with energies of tens keV can strongly affect the radiation belt boundary.",signatures:"Vladimir I. Sotnikov",downloadPdfUrl:"/chapter/pdf-download/78788",previewPdfUrl:"/chapter/pdf-preview/78788",authors:[{id:"97711",title:"Dr.",name:"Vladimir I.",surname:"Sotnikov",slug:"vladimir-i.-sotnikov",fullName:"Vladimir I. Sotnikov"}],corrections:null},{id:"78629",title:"Free-electron Driven Terahertz Wave Sources Based on Simth-Purcell Effect",doi:"10.5772/intechopen.100010",slug:"free-electron-driven-terahertz-wave-sources-based-on-simth-purcell-effect",totalDownloads:160,totalCrossrefCites:0,totalDimensionsCites:0,hasAltmetrics:0,abstract:"Terahertz electromagnetic wave is one of the hottest research topics in nowadays scientific world thanks to its broad applications in material characterization, medical imaging, wireless communication, and security checking etc. Using free-electron beams to interact with periodic structures via the famous Smith-Purcell effect is an efficient way of generating high-power terahertz radiation. In this chapter, we introduce the basic theory and latest developments of the terahertz radiation schemes using a free-electron beam (including continuous electron beam, a single electron bunch, and a train of electron bunches, etc.) to interact with periodic electromagnetic structures, including grating, surface plasmonics, and subwavelength hole arrays, via a special Smith-Purcell effect or Cherenkov-like effect. A kind of free-electron lasers based on the special Smith-Purcell radiation in the terahertz region is proposed and investigated, which can be developed as high-power terahertz wave sources for practical applications.",signatures:"Weihao Liu, Zijia Yu and Zhi Tao",downloadPdfUrl:"/chapter/pdf-download/78629",previewPdfUrl:"/chapter/pdf-preview/78629",authors:[{id:"356338",title:"Prof.",name:"Weihao",surname:"Liu",slug:"weihao-liu",fullName:"Weihao Liu"},{id:"427745",title:"Ms.",name:"Zijia",surname:"Yu",slug:"zijia-yu",fullName:"Zijia Yu"},{id:"427746",title:"Ms.",name:"Zhi",surname:"Tao",slug:"zhi-tao",fullName:"Zhi Tao"}],corrections:null},{id:"77873",title:"New Types of Dissipative Streaming Instabilities",doi:"10.5772/intechopen.98901",slug:"new-types-of-dissipative-streaming-instabilities",totalDownloads:80,totalCrossrefCites:0,totalDimensionsCites:0,hasAltmetrics:0,abstract:"Two new, previously unknown types of dissipative streaming instabilities (DSI) are substantiated. They follow from new approach, which allows solving in general form the classical problem of an initial perturbation development for streaming instabilities (SI). SI is caused by relative motion of the streams of plasma components. With an increase in level of dissipation SI transforms into a DSI. The transformation occurs because dissipation serves as a channel for energy removal for the growth of the negative energy wave of the stream. Until recently, only one type of DSI was known. Its maximal growth rate depends on the beam density nb and the collision frequency ν in the plasma as ∼nb/ν. All types of conventional beam-plasma instabilities (Cherenkov, cyclotron, etc.) transform into it. The solution of the problem of the initial perturbation development in systems with weak beam-plasma coupling leads to a new type of DSI. With an increase in the level of dissipation, the instability in these systems transforms to the new DSI. Its maximal growth rate is ∼nb/ν. The second new DSI develops in beam-plasma waveguide with over-limiting current of e-beam. Its growth rate ∼nb/ν. In addition, the solutions of abovementioned problem provide much information about SI and DSI, significant part of which is unavailable by other methods.",signatures:"Eduard V. Rostomyan",downloadPdfUrl:"/chapter/pdf-download/77873",previewPdfUrl:"/chapter/pdf-preview/77873",authors:[{id:"235189",title:"Prof.",name:"Eduard V.",surname:"Rostomyan",slug:"eduard-v.-rostomyan",fullName:"Eduard V. Rostomyan"}],corrections:null},{id:"78559",title:"Numerical Investigations of Electromagnetic Oscillations and Turbulences in Hall Thrusters Using Two Fluid Approach",doi:"10.5772/intechopen.99883",slug:"numerical-investigations-of-electromagnetic-oscillations-and-turbulences-in-hall-thrusters-using-two",totalDownloads:140,totalCrossrefCites:0,totalDimensionsCites:0,hasAltmetrics:0,abstract:"The first part of the contributed chapter discuss the overview of electric propulsion technology and its requirement in different space missions. The technical terms specific impulse and thrust are explained with their relation to exhaust velocity. The shortcoming of the Hall thrusters and its erosion problems of the channel walls are also conveyed. The second part of the chapter discuss the various waves and electromagnetic instabilities propagating in a Hall thruster magnetized plasma. The dispersion relation for the azimuthal growing waves is derived analytically with the help of magnetohydrodynamics theory. It is depicted that the growth rate of the instability increases with magnetic field, electron drift velocity and collisional frequency, whereas it is decreases with the initial drift of the ions.",signatures:"Sukhmander Singh, Bhavna Vidhani and Ashish Tyagi",downloadPdfUrl:"/chapter/pdf-download/78559",previewPdfUrl:"/chapter/pdf-preview/78559",authors:[{id:"282807",title:"Dr.",name:"Sukhmander",surname:"Singh",slug:"sukhmander-singh",fullName:"Sukhmander Singh"},{id:"421908",title:"Mr.",name:"Ashish",surname:"Tyagi",slug:"ashish-tyagi",fullName:"Ashish Tyagi"},{id:"421909",title:"Mrs.",name:"Bhavna",surname:"Vidhani",slug:"bhavna-vidhani",fullName:"Bhavna Vidhani"}],corrections:null},{id:"77778",title:"The Emerging Field Trends Erosion-Free Electric Hall Thrusters Systems",doi:"10.5772/intechopen.99096",slug:"the-emerging-field-trends-erosion-free-electric-hall-thrusters-systems",totalDownloads:129,totalCrossrefCites:0,totalDimensionsCites:0,hasAltmetrics:0,abstract:"The Hall-type accelerator with closed Hall current and open (that is unbounded by metal or dielectric) walls was proposed and considered both theoretically and experimentally. The novelty of this accelerator is the use of a virtual parallel surface of the anode and the cathode due to the principle of equipotentialization of magnetic field lines, which allows to avoid sputtering of the cathode surface and preserve the dynamics of accelerated ions. The formation of the actual traction beam should be due to the acceleration of ions with the accumulated positive bulk charge. A two-dimensional hybrid model in cylindrical coordinates is created in the framework of which the possibility of creation a positive space charge at the system axes is shown. It is shown that the ions flow from the hump of electrical potential can lead to the creation of a powerful ion flow, which moves along the symmetry axis in both sides from the center.",signatures:"Iryna Litovko, Alexey Goncharov, Andrew Dobrovolskyi and Iryna Naiko",downloadPdfUrl:"/chapter/pdf-download/77778",previewPdfUrl:"/chapter/pdf-preview/77778",authors:[{id:"238183",title:"Dr.",name:"Irina",surname:"Litovko",slug:"irina-litovko",fullName:"Irina Litovko"},{id:"238955",title:"Prof.",name:"Alexey",surname:"Goncharov",slug:"alexey-goncharov",fullName:"Alexey Goncharov"},{id:"356530",title:"Dr.",name:"Andrew",surname:"Dobrovolskii",slug:"andrew-dobrovolskii",fullName:"Andrew Dobrovolskii"},{id:"356532",title:"Ms.",name:"Iryna",surname:"Naiko",slug:"iryna-naiko",fullName:"Iryna Naiko"}],corrections:null},{id:"78592",title:"Gyrotron: The Most Suitable Millimeter-Wave Source for Heating of Plasma in Tokamak",doi:"10.5772/intechopen.98857",slug:"gyrotron-the-most-suitable-millimeter-wave-source-for-heating-of-plasma-in-tokamak",totalDownloads:127,totalCrossrefCites:0,totalDimensionsCites:0,hasAltmetrics:1,abstract:"In this chapter, brief outline is presented about gyro-devices. Gyro-devices comprise of a family of microwave devices and gyrotron is one among those. Various gyro devices, namely, gyrotron, gyro-klystron and gyro traveling-wave tubes (gyro-TWT) are discussed. Gyrotron is the only microwave source which can generate megawatt range of power at millimeter-wave and sub-millimeter-wave frequency. Gyrotron is the most suitable millimeter wave source for the heating of plasma in the Tokamak for the controlled thermoneuclear fusion reactors. This device is used both for the electron cyclotron resonance heating (ECRH) as well as for the electron cyclotron current drive (ECCD). In this chapter, the basic theory of gyrotron operation are presented with the explanation of various sub-systems of gyrotron. The applications of gyrotrons are also discussed. Also, the present state-of-the-art worldwide scenario of gyrotrons suitable for plasma heating applications are presented in details.",signatures:"Santanu Karmakar and Jagadish C. 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1. Introduction
Participants in the International Laboratory Accreditation Cooperation (ILAC) Mutual Recognition Agreement (MRA) recognize the calibration or test results obtained by each other’s accredited calibration and testing laboratories [1, 2, 3, 4]. ILAC Policy and Procedural publications are for the operation of the ILAC MRA. ILAC has a special policy for participation in proficiency testing activities, on metrological traceability of measurement results, for measurement uncertainty in calibration [5, 6, 7]. The policy for measurement uncertainty to base on the Guide to Uncertainty in Measurement (GUM) [8, 9, 10, 11] and retains the common understanding of the term calibration and measurement capabilities (CMCs) from the joint declaration issued by the International Bureau of Weights and Measures (BIPM) and ILAC [12]. ILAC has a special guideline for measurement uncertainty in testing [13]. This document provides guidance for the evaluation and reporting of measurement uncertainty in testing accordance with the requirements of the International Standard ISO/IEC 17025 [14].
National accreditation agencies in different countries have set quite strict requirements for accreditation of testing and calibration laboratories. Laboratory accreditation criteria in most accreditation systems include three main groups: laboratory technical equipment, personnel competence, and the effectiveness of the quality system. Interlaboratory comparisons (ILCs) are a form of experimental verification of laboratory activities to determine technical competence in a particular activity. Successful results of conducting ILCs for the laboratory are a confirmation of competence in carrying out certain types of measurements by a specific specialist on specific equipment.
To obtain reliable results of ILC accredited laboratories, it is necessary to improve the methods of processing these results. These methods are based on various data processing algorithms as required by international and regional guidelines and standards. To conduct ILC for CLs, it is necessary to take into account the relevant requirements of the international standards ISO/IEC 17025 [14] and ISO/IEC 17043 [15]. Therefore, it is necessary to choose the most optimal method of processing the obtained data, which would have a minimum number of restrictions on the application and allow to obtain reliable results. In addition, it is necessary to take into account the peculiarities of the calibration laboratories (CLs) when evaluating the results of ILС. Such features are related to the need to provide calibration of measuring instruments for testing laboratories.
ILCs for CLs are held nationally in different countries. Such ILCs are carried out to establish the competence of the CLs in calibrating various measuring instruments and working standards for various measured quantities [16, 17, 18, 19, 20, 21, 22, 23, 24]. For their implementation, various calibration objects are used. To evaluate the ILC data, various methods of their data processing are used [25, 26, 27, 28, 29, 30], and to estimate the measurement uncertainty, the regional guidance EA-04/02 М [31] is additionally used, in addition to the ILAC documents [8, 13]. However, in addition to the method of data evaluation, it is necessary to take into account other influencing factors on the CL result of ILC. In particular, unsatisfactory ILC results for all participating CLs may be associated with a large time drift of the calibrated measuring instrument.
The growing practical need of ILCs for CLs to ensure recognition of the obtained results at both national and international levels underscores the relevance of this research.
2. The national interlaboratory comparisons for calibration laboratories
The main purpose of accredited CLs is to calibrate working standards and measuring instruments for accredited testing laboratories. Significantly more testing laboratories are accredited by national accreditation bodies than CLs. For example, at the middle of 2021, 837 testing and 35 calibration laboratories were accredited in Ukraine. This represents only 4% of accredited CLs of the total number of all accredited laboratories. Therefore, the number of ILCs for testing laboratories is objectively much larger than for CLs.
The State Enterprise “Ukrmetrteststandard” (Ukraine) as a referent laboratory (RL) organized and carry out seven ILCs for accredited CLs from 2016 to 2019 [32, 33, 34, 35, etc]. The list of these ILCs is shown in Table 1. The calibration objects for these ILCs were working standards and measuring instruments for electrical quantities, and time and frequency. When carrying out comparisons, CLs calibrated objects in accordance with the requirements of the international standard ISO/IEC 17025 [14]. The total number of calibration object parameters ranged from 3 to 12. The total number of CLs with RL that took part in these comparisons ranged from 5 to 10.
ILC
Calibration object
Number of parameters
Number of participants
Period of carrying out
ILC1
Precision measuring thermocouple
AC voltage at 5 frequencies
5 labs
2016–2018
ILC2
Measures of electrical resistance (1th round)
3 nominations of resistance
8 labs
2016
ILC3
Measures of electrical resistance (2th round)
3 nominations of resistance
5 labs
2018–2019
ILC4
Precision measure of electric power
6 power factors at 2 frequencies
8 labs
2016–2018
ILC5
Low frequency signal generator
AC voltage at one frequency, total harmonic factor at 4 frequencies, 5 frequencies
4 labs
2016
ILC6
Electronic stopwatch
3 time intervals
9 labs
2016
ILC7
High-frequency signal generator
3 frequencies
10 labs
2018
Table 1.
The list of national ILCs for CLs.
In all presented ILCs, the assigned value (AV) with its uncertainty was taken as the value with its uncertainty of the RL. This was done because the RL had the best measurement capabilities among all CLs that took part in the comparisons. For many years RL has taken part in international comparisons of national measurement standards of electrical quantities within the framework of Regional Metrological Organizations (COOMET, EURAMET, and GULFMET) and had positive results. RL also had published CMCs for some electrical quantities in the BIPM Key Comparison Database [36].
A program for all ILCs was implemented in accordance with the requirements of ISO/IEC 17043 [15]. CLs that participated in the ILCs performed calibration of the measuring instruments (calibration object) provided to the RL in accordance with their own methods according to the radial scheme [4]. RL sent the calibration object to the participating laboratory, and this laboratory returned this object back to RL. In this case, the RL constantly monitored the stability of the calibration object [35, 37]. The RL determined the characteristics of the instability of the calibration object before and after its research in the CLs participating in the ILC.
In accordance with the adopted ILC programs, RL analyzed the calibration data provided by the CLs [38], in particular, analyzed the declared measurement uncertainty. The data obtained from CLs were necessarily checked by RL for their consistency. Indicators for assessing of consistency were En and z indexes set and defined in [4, 15]. The general algorithm of processing of the received primary data of ILCs given in [34] was used. In case of inconsistent data, RL reported this appropriate CL and analyzed the responses received from this laboratory. RL prepared a report on the comparisons, evaluating the data of all CLs. In the event that the laboratory or laboratories received inconsistent results of comparisons, RL suggested that they take the necessary corrective action.
3. The traditional data evaluation of interlaboratory comparisons
The traditional assessment of ILC data for CLs is carried out in accordance with the requirements of ISO/IEC 17043 [15]. During of the evaluation of primary data from the participating CLs, the interlaboratory deviation of the measurement results or degree of equivalences (DoE) was calculated based on the ILCs results.
The DoE for j-th CLs participant of ILC is calculated using Equation [4, 34, 38].
Dlabj=xlabj−XAV,E1
where xlabj is measured value for i-th CL; XAV is AV for ILC.
Expanded uncertainty of the result of each participant Uxlabj and expanded uncertainty of AV UXAV were used to check the consistency of the primary ILC data and to calculate En index (En number) using equation
On Figures 1–3 show the traditional graphical interpretation of the results of three ILCs at one of the calibration points (ILC 2–1, Figure 1, ILC 4–2, Figure 2 and ILC 6–1, Figure 3 respectively). The evaluation of primary data of all ILCs is carried out by means of the specially developed software “Interlaboratory comparisons” (Ukraine) which implements the algorithm presented in [34]. To prepare reports on ILCs, RL used specified software that allowed calculating the En and z indexes and constructing a graphical display of the results. The figures show the DoE with expanded uncertainty for all participating CLs in ILCs. The green dashed line shows the measurement uncertainty limits of the AV of ILC.
Figure 1.
DoE of CLs for ILC 2–1.
Figure 2.
DoE of CLs for ILC 4–2.
Figure 3.
DoE of CLs for ILC 6–1.
Only two laboratories (lab 4 and lab 6 for ILC 2–1) have an unsatisfactory result for two ILCs using the En index. En index more characterizes the reliability of measurement results of laboratories participating in the ILC, but is not always sufficient to determine the accuracy of measurement results.
4. The additional data evaluation of interlaboratory comparisons
The consistency evaluation of data using En and z indicators is important not only to confirm the technical competence of laboratories participating in the ILC. This will also help to increase the accuracy of calibration by the laboratory participating in the ILC with a corresponding reduction in measurement uncertainty.
The z index compares the measurement results of all laboratories with each other and gives better information about the accuracy of measurements in laboratory. The measurement accuracy is an important characteristic for CL, therefore this index is more suitable for evaluating ILC data for CLs.
z index (z score) is calculated by the equation
z=Dlabj/σ,E3
where σ is the standard deviation for qualification assessment (ILC).
|z| ≤ 2.0 indicates a satisfactory performance characteristic and does not require adjustment or response measures, 2.0 < |z| < 3.0 indicates a dubious performance characteristic and requires precautionary measures, and |z| ≥ 3.0 indicates an unsatisfactory performance characteristic and requires adjustment or response measures.
In Tables 2–8 shows the calculated results of En and z indexes at all points of the calibration for all ILCs. En and z indexes are zero for RL. Cells with unsatisfactory results are highlighted in grey in the tables. An unsatisfactory result is the excess for En index of the value 1, and for the z index of 2 (does not require adjustment or response measures) or 3 (requires adjustment or response measures) [4, 15].
ILC data
Index
Lab 1
Lab 2
Lab 3
Lab 4
ILC1–1
En
−0.854
0.444
0.438
−0.312
z
−0.584
0.114
0.224
−2.462
ILC1–2
En
−0.451
0.818
1.522
−0.064
z
−1.146
0.266
0.605
−2.090
ILC1–3
En
−0.645
0.882
0.987
0.022
z
−1.167
0.483
0.781
1.895
ILC1–4
En
−0.147
0.238
0.129
0.452
z
−0.025
0.019
0.018
2.503
ILC1–5
En
—
0.753
0.382
—
z
—
2.265
1.939
—
Table 2.
Results of ILCs for calibration of precision measuring thermocouple.
ILC data
Index
Lab 1
Lab 2
Lab 3
Lab 4
Lab 5
Lab 6
Lab 7
ILC2–1
En
0.249
−0.245
−0.008
−4.631
−0.100
2.352
−0.021
z
2.677
−0.027
−0.996
−0.208
−0.005
0.188
−0.169
ILC2–2
En
−1.955
6.066
−0.018
−0.814
0.256
−0.646
−0.032
z
−2.404
0.880
−1.460
−0.197
0.056
−0.253
−1.460
ILC2–3
En
−0.899
4.179
−0.086
0.171
−0.470
0.975
−0.058
z
−2.251
1.318
−0.969
0.051
−0.127
0.367
−0.969
Table 3.
Results of ILCs for calibration of measures of electrical resistance (1-th round).
ILC data
Index
Lab 1
Lab 2
Lab 3
Lab 4
ILC3–1
En
0.301
0.133
0.367
0.322
z
0.117
2.658
0.152
0.961
ILC3–2
En
0.194
0.065
0.042
0.051
z
0.012
2.579
0.004
0.457
ILC3–3
En
0.301
0.133
0.367
0.322
z
0.117
2.658
0.152
0.961
Table 4.
Results of ILCs for calibration of measures of electrical resistance (2-th round).
ILC data
Index
Lab 1
Lab 2
Lab 3
Lab 4
Lab 5
Lab 6
ILC4–1
En
0.000
0.004
0.001
−0.013
0.000
0.000
z
0.002
0.215
0.029
−2.804
0.018
0.018
ILC4–2
En
0.000
0.002
0.002
0.034
0.000
0.000
z
0.001
0.046
0.046
2.875
0.004
0.006
ILC4–3
En
0.000
0.002
0.001
0.000
0.000
0.000
z
0.157
2.683
0.679
−0.192
−0.105
0.157
ILC4–4
En
0.000
0.002
0.001
0.000
0.000
0.000
z
0.207
2.657
1.055
−0.170
−0.075
0.207
ILC4–5
En
0.000
0.002
−0.001
0.119
0.000
0.000
z
0.001
0.013
−0.009
2.859
0.000
0.001
ILC4–6
En
0.000
0.002
0.002
0.137
0.000
0.000
z
0.000
0.012
0.012
2.862
0.000
0.001
ILC4–7
En
0.000
0.003
0.003
0.000
0.000
0.000
z
−0.043
2.260
1.919
−0.043
0.000
−0.043
ILC4–8
En
0.000
0.001
0.001
0.000
0.000
0.000
z
0.176
2.439
2.187
0.176
0.553
0.176
ILC4–9
En
0.001
0.002
0.000
0.000
0.000
0.001
z
0.532
2.787
0.622
−0.009
−0.099
0.532
ILC4–10
En
0.000
0.002
0.000
0.000
−0.001
0.000
z
0.108
2.570
0.569
−0.277
−0.354
0.108
ILC4–11
En
0.001
0.002
0.002
0.000
0.000
0.001
z
0.331
2.462
2.068
0.095
0.253
0.331
ILC4–12
En
0.001
0.002
0.001
0.000
0.000
0.001
z
0.498
2.989
1.329
0.406
0.406
0.498
Table 5.
Results of ILCs for calibration of precision measure of electric power.
ILC data
Index
Lab 1
Lab 2
Lab 3
ILC5–1
En
−0.235
−0.014
−0.305
z
−2.479
−0.077
−1.044
ILC5–2
En
−0.050
−0.056
0.036
z
−1.095
−1.461
1.095
ILC5–3
En
0.040
0.000
0.035
z
1.206
0.000
2.412
ILC5–4
En
0.074
0.033
0.068
z
1.414
1.414
2.828
ILC5–5
En
0.737
0.397
0.139
z
2.399
2.181
0.727
ILC5–6
En
−0.087
−0.055
−0.016
z
−2.557
−1.627
−0.465
ILC5–7
En
0.289
0.278
0.122
z
2.448
2.292
1.011
ILC5–8
En
−0.086
0.016
−3.258
z
−0.063
0.012
−2.326
ILC5–9
En
−0.284
−0.061
0.029
z
−2.315
−0.489
0.233
ILC5–10
En
−0.947
−1.024
0.692
z
−1.335
−1.442
0.975
Table 6.
Results of ILCs for calibration of low frequency signal generator.
ILC data
Index
Lab 1
Lab 2
Lab 3
Lab 4
Lab 5
Lab 6
Lab 7
Lab 8
Lab 9
ILC6–1
En
0.713
−0.212
0.992
0.379
0.894
0.328
0.897
−0.290
0.982
z
1.811
−0.075
0.503
0.302
0.503
0.365
3.245
−0.176
0.415
ILC6–2
En
0.998
−0.943
0.733
0.218
0.676
0.161
0.192
−0.379
0.914
z
3.160
−0.334
0.486
0.729
0.790
0.501
1.686
−0.273
1.413
ILC6–3
En
0.711
−0.587
0.459
0.157
0.296
0.065
0.804
−0.273
0.754
z
2.008
−0.193
0.468
0.908
0.468
0.289
3.012
−0.165
1.582
Table 7.
Results of ILCs for calibration of electronic stopwatch.
ILC data
Index
Lab 1
Lab 2
Lab 3
Lab 4
Lab 5
Lab 6
Lab 7
Lab 8
Lab 9
Lab 10
ILC7–1
En
0.050
0.662
−0.072
−0.025
0.643
−0.164
−0.384
−0.039
−0.012
−0.124
z
1.243
2.666
−0.687
−0.634
0.857
−0.124
−0.588
−0.631
−0.118
−0.433
ILC7–2
En
0.067
0.912
−0.076
−0.034
0.775
−0.253
−0.475
−0.068
0.005
−0.052
z
1.261
2.533
−0.695
−0.629
0.761
−0.182
−0.725
−1.040
0.034
−0.145
ILC7–3
En
0.062
1.134
−0.072
−0.053
0.164
−0.160
−0.648
−0.042
−0.014
−0.104
z
1.045
2.847
−0.746
−0.834
0.164
−0.131
−0.574
−0.427
−0.09
−0.276
Table 8.
Results of ILCs for calibration of high-frequency signal generator.
Оn Figure 4 shows the graphical interpretation of the results of estimation of En (a) and z (b) indexes for ILC 2–1, on Figure 5 – for ILC 4–2, and in Figure 6 – for ILC 6–1, respectively.
Figure 4.
Values of En and z indexes for ILC 2–1: a is En index, b is z index.
Figure 5.
Values of En and z indexes for ILC 4–2: a is En index, b is z index.
Figure 6.
Values of En and z indexes for ILC 6–1: a is En index, b is z index.
5. The summarized results of interlaboratory comparisons
The summarized results of estimation of En and z indexes for all ILCs are shown in Table 9 and Figure 7. The percentage of discrepancies two assessments for ILCs 1, 3, 4 and 6 estimates are 100, for ILCs 2, 5 and 7 estimates are from 95 to 97. This suggests that the conclusions that can be drawn about the technical competence of the laboratories participating in these ILCs are completely inconsistent.
The summarized results of estimation of En and z indexes for all ILCs.
Without RL.
Figure 7.
The summarized results of estimation of En and z indexes for all ILCs: a is absolute value, b is percentage value (%).
Only one result of ILC1 according to En index have inconsistency (lab 3). At the same time, 4 results of ILC1 according to z indexes have inconsistencies (lab 2 and lab 4).
5 results of ILC2 according to En indexes have inconsistencies (for labs 1, 2, 4 and 6). At the same time, 3 results of ILC2 according to z indexes have inconsistencies (only for lab 1).
ILC3, ILC4, and ILC6 according to En index have no inconsistencies. At the same time, 3 results of ILC3 according to z indexes have inconsistencies (only for lab 2), 14 results of ILC4 according to z indexes have inconsistencies (for labs 2, 3 and 4), and 4 results of the ILC6 according to z indexes have inconsistencies (for labs 2, 3, and 4), including 3 from 4 are very large (z > 3.0).
Only one ILC7 result according to En index have inconsistency (for lab 2). At the same time, 3 results of the ILC7 according to z indexes have inconsistencies (for lab 2 also).
The results of the data consistency analysis show that all ILCs, taking into account both indexes, have measurement points with unsatisfactory results. Analysis of the data taking into account the En index shows that only three ILCs (ILC3, ILC4, and ILC6) have satisfactory results. At the same time, analysis of the data taking into account the z index (z > 2) shows that all ILCs have measurement points with unsatisfactory results. ILС6 has measurement points with significantly unsatisfactory results, taking into account the z index (z > 3).
If we return to the analysis of Figures 1–3, it can be seen that lab 4 for ILCs 2–1 and lab 1 and lab 7 for ILC6–1 have very large declared measurement uncertainties with large DoEs. This led to unsatisfactory results, taking into account the z index. The main reason for the unsatisfactory result of lab 3 for ILCs 1–2, taking into account En index, is, on the contrary, a very small declared measurement uncertainty.
The general recommendation for lab 3 and lab 4 for ILC1–2, as well as for lab 4 for ILC4–2, and lab 1 and lab 7 for ILC6–1 is to revise the estimate of the measurement uncertainty, taking into account guides [8, 31]. This measurement uncertainty can be influenced by both the calibration results of the laboratory working standards and the level of competence of the laboratory personnel. Taking these recommendations into account can improve the results of that laboratories participation in other rounds of ILCs or new ILCs.
6. The influence of travelling standards instability
The travelling standards instability can affect the results of ILCs for CLs. Some works are devoted to assessing its influence, in particular compensation for its instability. The repeatability of a good measuring instrument is below 10% of its maximum error as shown in [39]. The travelling standard with 0,2% shows variations of random errors below x˜±0.02% where x˜ is the average of the readings during calibration. This a small Type A uncertainty in relation to other components is show.
Typically, RL already takes into account the travelling standards instability in the ILC assigned value XAV and its expanded uncertainty [4].
UXAV=2⋅u2xref+u2xinst,E4
where uxref is the standard measurement uncertainty obtained by calibrating of travelling standard with a RL; uxinst is the standard measurement uncertainty from the travelling standard instability of during ILC period
uxinst=ΔXmax/3,E5
ΔXmax is the maximum change in nominal value of travelling standard during ILC period.
The absence of a significant effect of the travelling standards instability on the evaluation of the CL result in the ILC can be at its maximum instability, which is determined by the expression [39].
xinst≤U2xlabj+U2XAV.E6
The value of the travelling standards instability can be obtained for several cases: measurements of the RL of the travelling standard in the process of carry out of ILC; from the technical specification for the travelling standard, measurements of the RL of the travelling standard for a long time, and etc. Results of calculating the En index for various options for accounting for travelling standards instability are shows in [39].
In any case, from expression (4) it follows that with an increase in the value of the measurement uncertainty associated with instability, the value of the En index only decreases. In this case, it can be stated that the use of a more unstable travelling standard can improve the consistency of the ILC data, which is not acceptable for CL. To carry out ILСs for CLs, it is more preferable to use working standards as calibration objects. Typically, a working standard has less instability than a measuring instrument. The use of a measuring instrument as a travelling standard can lead to somewhat distorted results of such ILCs.
An analysis RL of the travelling standard instability for all calibration points of the ILC7 is given in [33]. The drift of travelling standard for ILC7 at all frequencies is presented on Figure 8. The uncertainty of travelling standards instability for ILC7 is presented in Table 10. The contribution of the uncertainty from the long-term drift of the travelling standard to the standard uncertainty of AV for the entire duration of ILC7 is from 5.3 to 8.3% for all calibration points. Such a drift of the measuring instrument used as a calibration object is acceptable for the ILC. It does not distort the ILC results for the participating CLs.
Figure 8.
The drift of travelling standard for ILC7: a is frequency 130 MHz, b is frequency 168 MHz, c is frequency 223 MHz.
ILC7 point
Frequency (MHz)
uXAV (Hz)
uxinst (Hz)
Drift contribution to uncertainty AV (%)
ILC7–1
130
0.12
0.01
8.3
ILC7–2
168
0.17
0.01
5.9
ILC7–3
223
0.19
0.01
5.3
Table 10.
The uncertainty of travelling standards instability for ILC7.
The list of travelling standard for all ILCs and values of En and z indexes are shown in Table 11.
ILC
Calibration object
Working standard
Measuring instrument
En index
z index
Unsatisfactory (%)
ILC1
Precision measuring thermocouple
Yes
No
5
20
ILC2
Measures of electrical resistance (1th round)
Yes
No
24
14
ILC3
Measures of electrical resistance (2th round)
Yes
No
0
25
ILC4
Precision measure of electric power
Yes
No
0
19
ILC5
Low frequency signal generator
No
Yes
7
33
ILC6
Electronic stopwatch
No
Yes
0
45
ILC7
High-frequency signal generator
No
Yes
3
13
Table 11.
The list of travelling standard for ILCs and values of En and z indexes.
The use of a measuring instrument as a calibration object leads to a slight increase in the values of the z index and practically does not affect the En index, as can be seen from Table 11.
7. The improvement of the evaluation of interlaboratory comparison results
Statistical methods for use in proficiency testing by ILCs are presented in [26, 27]. The aim of creating alternative statistics in order to improve the analysis and evaluation of ILC measurement results is research work [40]. The improvement of statistical indicators is proposed by addressing two specific issues: robustness and reliability. The proposed methodology is not traditional for ILC, but it can be used as an additional methodology for checking the results of ILC.
The following conditions are provided for data evaluation of international comparison of national standards: the travelling measurement standard is stable, the measurement results presented by laboratories are reciprocally independent, and the Gaussian distribution is assigned to a measurand in each laboratory [41, 42, 43, 44]. The same conditions can be extended for data evaluation of ILCs for CLs. Frequently the measurement procedures for supplementary comparisons of national standards [44] are the calibration procedures of these laboratories. Such calibration procedures can also be extended to ILCs for CLs. In such a case, the calibration capabilities of the laboratory can be confirmed.
The application of z index for evaluation of CL results recommended instead of En index since this number is not applicable due to the difficulty in determining the AV [16]. Of course, for accredited test laboratories, it is preferable to use the services of a CL with the best calibration capabilities. Better calibration capabilities of laboratories are characterized by lower calibration uncertainties of working standards and measuring instruments. CLs with a satisfactory value of the En index in the ILC, but having large calibration uncertainties become uncompetitive. If we return to the analysis of Figures 1–3, it can be seen that lab 1, 3 and 7 for ILCs 1–2, lab 4 for ILC4–2, and lab 1 and lab 7 for ILC6–1 have very large declared measurement uncertainties.
The declared measurement uncertainties of CL for ILC are judged as confirmed if the following equation is satisfied [4, 43].
Dlabj<2uDlabj.E7
In case the declared uncertainties CL don’t confirmed during the ILC and for their confirmation it is necessary to participate in other similar ILCs.
Often, a national metrological institute or an accredited CL, which is an RL in ILC, performs high-precision calibration of working standards and measuring instruments for CLs participating in this ILC. In this case, a correlation of the obtained CL results is formed, which must be taken into account when evaluating the data of such an ILC. Covariance’s are estimated by careful analysis of the uncertainty budget of CLs by the RL
covxlabjXAV=u02,E8
where u02 is common input to the uncertainty budgets of both results [43].
In this case, the value of the En index is calculated by the formula:
En=Dlabj/U2xlabj+U2XAV−2covxlabjXAV.E9
If the value of the En index meets the specified requirement (≤ 1.0), then the minimum standard measurement uncertainty, that can be claimed as calibration capability of CL participating in ILC, is:
uCCxlabj=uILCxlabj.E10
If the value of the En index not meets the specified requirement (> 1.0), then the minimum standard measurement uncertainty, that can be claimed as calibration capability of CL participating in ILC, is:
uCCxlabj=Dlabj24+u2XAV,E11
where uXAV is the standard measurement uncertainty of AV.
Correspondingly, the extended uncertainty is U0.95xlabj=2uILCxlabj .
The same requirements can be extended for compliance (≤ 2.0) or inconsistency (> 2.0) of the value of the z index with the established requirements. In this case, the minimum standard measurement uncertainty, that can be claimed as calibration capability of CL participating in ILC, will be determined by formulas (10) and (11), respectively.
If the standard uncertainty uXAV of the AV is too large in comparison with the standard deviation σ for ILC, then there is a risk that some laboratories will receive action and warning signals because of inaccuracy in the determination of the AV, not because of any cause within the laboratories. If
uXAV≤0.3σE12
then the uncertainty of the AV is negligible and need not be included in the interpretation of the ILC results. Further, all CLs participating in ILC shall carry out the same number of replicate measurements. This approach assumes that CLs have generally similar repeatability [26].
To evaluate the ILC data, can use z′ index also [26] which calculated by the equation
z′=Dlabj/σ2+u2XAVE13
This equation may be used when the AV is not calculated using the results reported by CLs participating in ILC. z′ index shall be interpreted in the same way as z index and using the same critical values of 2.0 and 3.0.
Comparison of the equations for z and z′ indexes shows that z′ index for ILC will all be smaller than the corresponding z index by a constant factor of σ/σ2+u2XAV .
When the inequality established by expression (12) is satisfied, then this factor will fall in the range: 0.96≤σ/σ2+u2XAV≤1.00. In this case, z′ index will be nearly identical to z index, and it may be concluded that the uncertainty of the AV is negligible. When the inequality established by expression (12) is not satisfied, the difference in magnitude of the z′ and z indexes may be such that some z index exceeds the critical values of 2.0 or 3.0.
8. Conclusions
To perform an ILC for CLs, RL must provide a stable working standard or measuring instrument as a calibration object and monitor its drift throughout the ILC. The use of a measuring instrument as a calibration object leads to a slight increase in the values of the z index and practically does not affect the En index. The application of z index for evaluation of CL results recommended instead of En index.
The analysis of the results of the ILC for CLs for consistency should include not only the analysis of the values of the En index, but also the z index. If we restrict ourselves to only the En index, then it is possible to get unreliable results of the ILC and not identify problems in the CL-participants of the ILC. In 3 from 7 ILCs examined, the En index showed completely satisfactory results, while the z index in all of these 3 ILCs revealed problematic results from the participating laboratories.
The stable travelling standard, the independent measurement results of laboratories with Gaussian distribution are main conditions for data evaluation of ILC for CLs. To participate in the ILC when declaring its measurement uncertainty, CLs must conduct a thorough analysis of the components of this uncertainty. It is necessary to take into account the correlation of the laboratory data of the participants of the ILC when evaluating its results. Covariance is estimated by carefully analyzing the CL uncertainty budget using RL.
The minimum standard measurement uncertainty that can be claimed as the calibration capability of a CL participating in an ILC can be determined in different ways depending on the value of the obtained En index or z index. If the standard uncertainty of AV is too large compared to the standard deviation for the ILC, there is a risk of unreliable results for some CLs.
\n',keywords:"interlaboratory comparison, data evaluation, referent laboratory, calibration laboratory, calibration, measurement uncertainty",chapterPDFUrl:"https://cdn.intechopen.com/pdfs/78194.pdf",chapterXML:"https://mts.intechopen.com/source/xml/78194.xml",downloadPdfUrl:"/chapter/pdf-download/78194",previewPdfUrl:"/chapter/pdf-preview/78194",totalDownloads:125,totalViews:0,totalCrossrefCites:0,totalDimensionsCites:0,totalAltmetricsMentions:0,impactScore:0,impactScorePercentile:21,impactScoreQuartile:1,hasAltmetrics:0,dateSubmitted:"June 24th 2021",dateReviewed:"July 16th 2021",datePrePublished:"August 21st 2021",datePublished:"May 11th 2022",dateFinished:"August 21st 2021",readingETA:"0",abstract:"National accreditation agencies in different countries have set quite strict requirements for accreditation of testing and calibration laboratories. Interlaboratory comparisons (ILCs) are a form of experimental verification of laboratory activities to determine technical competence in a particular activity. Successful results of conducting ILCs for the laboratory are a confirmation of competence in carrying out certain types of measurements by a specific specialist on specific equipment. To obtain reliable results of ILC accredited laboratories, it is necessary to improve the methods of processing these results. These methods are based on various data processing algorithms. Therefore, it is necessary to choose the most optimal method of processing the obtained data, which would allow to obtain reliable results. In addition, it is necessary to take into account the peculiarities of the calibration laboratories (CLs) when evaluating the results of ILС. Such features are related to the need to provide calibration of measuring instruments for testing laboratories. The evaluation results for ILCs for CLs are presented. The results for all participants of ILCs were evaluated using the En and z indexes. The obtained results showed that for the such ILCs it is also necessary to evaluate the data using the z index also.",reviewType:"peer-reviewed",bibtexUrl:"/chapter/bibtex/78194",risUrl:"/chapter/ris/78194",book:{id:"10968",slug:"applied-aspects-of-modern-metrology"},signatures:"Oleh Velychko and Tetyana Gordiyenko",authors:[{id:"94982",title:"Prof.",name:"Tetyana",middleName:null,surname:"Gordiyenko",fullName:"Tetyana Gordiyenko",slug:"tetyana-gordiyenko",email:"T_Gord@hotmail.com",position:null,profilePictureURL:"https://mts.intechopen.com/storage/users/94982/images/279_n.jpg",institution:null},{id:"223340",title:"Prof.",name:"Oleh",middleName:null,surname:"Velychko",fullName:"Oleh Velychko",slug:"oleh-velychko",email:"velychko@hotmail.com",position:null,profilePictureURL:"https://mts.intechopen.com/storage/users/223340/images/system/223340.jpg",institution:null}],sections:[{id:"sec_1",title:"1. Introduction",level:"1"},{id:"sec_2",title:"2. The national interlaboratory comparisons for calibration laboratories",level:"1"},{id:"sec_3",title:"3. The traditional data evaluation of interlaboratory comparisons",level:"1"},{id:"sec_4",title:"4. The additional data evaluation of interlaboratory comparisons",level:"1"},{id:"sec_5",title:"5. The summarized results of interlaboratory comparisons",level:"1"},{id:"sec_6",title:"6. The influence of travelling standards instability",level:"1"},{id:"sec_7",title:"7. The improvement of the evaluation of interlaboratory comparison results",level:"1"},{id:"sec_8",title:"8. Conclusions",level:"1"}],chapterReferences:[{id:"B1",body:'ILAC B7:10/2015. The ILAC Mutual Recognition Arrangement, ILAC, 2015; 8 p.'},{id:"B2",body:'ILAC P4:05/2019. 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1. Introduction
Outer space offers several abnormal and/or unique environmental conditions, including microgravity, vacuum/hypovaria, acceleration, extreme temperature, space debris, space radiation, and confinement/isolation. As the latter four conditions may be mitigated by spacecraft engineering (i.e., pressurization and the bulkhead), we focused on microgravity and its effects on human physiology [1, 2, 3, 4, 5, 6, 7, 8].
In spaceflight, astronauts face three periods of physiological adaptation induced by changing gravity: (1) changes upon entry to microgravity (initial adaptation), (2) changes after prolonged exposure to microgravity, and (3) readaptation to 1 G gravity on Earth after returning from space. Body systems influenced by microgravity are the neurovestibular, cardiovascular, musculoskeletal, bone metabolic, and immuno-hematological systems. The changes associated with these systems occur during the adaptation phases outlined above. We will briefly discuss each of these body systems.
2. Neurovestibular system
2.1 Space motion sickness
How do we humans sense our relative positions in three-dimensional space? There are three sensory systems in the human body that help us define position: the visual, somatosensory, and vestibular systems. Most of the information from the outside world is processed by the visual system, but the combination of somatosensory and vestibular systems from the inner body helps define the positional status.
The vestibular organs include the otolith organs and semicircular canals. The otolith organs, saccules (sagittal direction) and utriculi (horizontal direction), sense linear acceleration. The semicircular canals, anterior, posterior, and horizontal, detect angular velocity of the head. The vestibular organs in the inner ear detect and measure linear and angular acceleration. These responses—already a complex set of signals—are further integrated with visual and proprioceptive inputs.
Exposure to microgravity alters some of these input signals, leading to misinterpretation and inadequate responses by the brain. This may cause vertigo, nausea, vomiting, appetite loss, headache, pallor, etc. As the symptoms are like those of motion sickness, this set of symptoms is termed “space motion sickness,” but unlike conventional motion sickness, antiemetic drugs cannot suppress the symptoms of space motion sickness. Approximately 60–80% of astronauts develop the symptoms within 2 or 3 days after launch. Space motion sickness is considered important because of its potential impact on the astronauts’ operational performance.
Although sensory misinterpretation may play a role in space motion sickness, its exact mechanism remains unknown. There are, however, several hypotheses: (1) sensory conflict, (2) fluid shift, (3) otolith asymmetry, and (4) orientation adaptation [9, 10].
The sensory conflict hypothesis suggests that loss of tilt-related otolith upon entry into microgravity causes a conflict between actual and anticipated signals from sense organs subserving spatial orientation. Such sensory conflicts are thought to induce motion sickness in other environments.
The fluid shift hypothesis suggests that space motion sickness results from the caudad fluid shifts, which in turn result from the hydrostatic pressure gradients in the lower body to the thoracic cavity or to the cranial cavity when entering microgravity. The cephalad fluid shift leads to visible puffiness in the face and is thought to increase the intracranial pressure, the cerebrospinal fluid pressure, or the inner ear fluid pressure, altering the response properties of the vestibular receptors and inducing space motion sickness.
The otolith asymmetry hypothesis is based on the theory that a mass difference in otolith between the left and right ear is the origin of space sickness and that there is interindividual susceptibility.
The otolith adaptation theory, or otolith tilt-translation reinterpretation theory, is the theory that space motion sickness is caused during the process of the brain learning to reinterpret novel otolith quasi-static signals to represent linear acceleration in space rather than the usual interpretation of tilt relative to the vertical direction on Earth.
Until now, it was unclear which of these theories (if any) was most likely. However, evidence from Space Shuttle missions suggests that the otolith asymmetry and otolith adaptation theories are unlikely.
2.2 Countermeasures for space motion sickness
In the Shuttle program and in the case of the International Space Station (ISS), the most commonly used countermeasure for space motion sickness is pharmacotherapy. Dornhoffer [11] reported the effects of four drug countermeasures (lorazepam, meclizine, promethazine, and scopolamine) for alleviating motion sickness induced by vestibular stimulation with a rotary chair and found that scopolamine was the only countermeasure to significantly change the mean duration of rotation compared with the placebo (p < 0.008), with a > 40% increase in rotation time.
In the Shuttle study, administration of promethazine at 20–50 mg was recommended by intramuscular injection or suppository. In the ISS study, meclizine and dimenhydrinate with cinnarizine were hypothesized to affect the medial vestibular nucleus. Promethazine is a vestibular suppressor, but a more recent report [12] demonstrated that d-amphetamine counters this suppression and inhibits the effects of fatigue on the saccadic reaction time.
We propose that artificial gravity is also effective in preventing space motion sickness because constant gravity on the otolith is effective against all four etiologies of this maladaptation.
3. Cardiovascular system
3.1 Effects of microgravity in the cardiovascular system
The changes in the cardiovascular system begin solely with the fluid shift associated with microgravity, followed by the decreased circulatory blood volume, cardiac size, and aerobic capacity, and the most prominent symptom, postflight orthostatic intolerance. These symptoms are generically known as “cardiovascular deconditioning” [13, 14, 15, 16, 17].
When the spacecraft reaches low Earth orbit (LEO), body fluids move from the lower body to the thorax, which is associated with the increase in the intraocular pressure and morphological alterations in the central nervous system, demonstrated by changes in the magnetic resonance imaging (MRI).
As a result of fluid shift, the leg volume decreases and the face becomes puffy. The leg volume decreases by 1 L, whereas subcutaneous tissue at the forehead thickens by as much as 7% compared with in the preflight supine position. The pulmonary capillary blood volume increases by approximately 25%, and intraocular pressure can nearly double. Fluid shift increases the cardiac volume and stroke volume at the beginning of the spaceflight (first 24 to 48 hours), but over time, the heart rate, stroke volume, and cardiac output stabilize to the preflight sitting level. The arterial blood pressure slightly decreases compared with the preflight level. Compared with “space motion sickness,” cardiovascular and fluid balance adaptation is gradual. The symptoms appear in 3–5 days and disappear after 1–2 weeks, causing facial edema, nasal stiffness, heavy headedness, papilledema, or jugular vein dilatation. These symptoms upon exposure to microgravity disappear at most 2 weeks after the reduction in circulatory plasma volume [13, 14, 15, 16, 17].
The cardiovascular changes in actual spaceflight differ from those in stimulations such as head-down bedrest or dry immersion. First, the volume of fluid shift is much larger than the orthostatic change from the supine to upright positions. The fluid volume loss during simulated microgravity (e.g., head-down bedrest or dry immersion) is less than 50% of that observed in actual spaceflight. Second, the central venous pressure measured during spaceflight does not increase as much as in head-down bedrest. Third, the diuresis caused during simulated microgravity is to a lower degree.
Then what is the cause of reduced blood volume after adaptation to microgravity? Diedrich et al. [18] explained the reduced blood volume in space as (1) a negative balance 2010 of decreased fluid intake and smaller reduction of urine output; (2) fast fluid shifts from the intravascular to interstitial spaces as a result of lower transmural pressure after reduced compression of all tissues by gravitational forces, especially of the thorax cage; and (3) fluid shifts from intravascular to muscle interstitial spaces because of lower muscle tone required to maintain body posture, and the attenuated diuresis during space flight is due to increased retention after stress-mediated sympathetic activation during the initial phase of space flight.
3.2 Decrease in the circulatory blood volume
The centralization of body fluid induces dehydration to adapt to the microgravity environment. The cephalad fluid shift causes an increase in venous return and marked increase in the stroke volume, inducing the alterations in the autonomic and endocrine systems to control the cardiovascular system.
On the first day of microgravity exposure, urine volume does not increase, but the circulatory blood volume suddenly decreases by 17%, probably due to the shift of water from the intravascular to the interstitial spaces and finally to the intracellular space. This induces an increase in the hematocrit level, which suppresses erythropoietin production and reduces the erythrocyte volume. Reductions in the circulatory plasma volume and erythrocyte volume equal an 11% reduction in the total blood volume, and this stabilizes the central blood volume to a new equilibrium, which nearly equals the central blood volume in the standing position at 1 G on Earth.
Upon the above alterations, the autonomic nervous system stabilizes the blood pressure by suppressing the sympathetic functions and activating the vagal functions by reducing the heart rate and suppressing muscle sympathetic nerve activity. Alterations include suppression of vasopressin by the Henry-Gauer reflex, facilitation of α-natriuretic peptide secretion, and suppression of the renin-angiotensin-aldosterone system, all of which facilitate urination. Thus, centralized body fluid is excreted, accounting for 10–15% of the circulatory blood volume, increased hematocrit level, and adaptation of the cardiovascular system 5–7 days after microgravity exposure. This ameliorates the facial edema and jugular distension. This adaptation causes cardiovascular deconditioning, including orthostatic intolerance, after returning to 1 G on Earth.
3.3 Reduced heart size
Once exposed to microgravity, the volume and pressure stimuli disappear. Constant postural change of lying down from upright standing on Earth loads intermittent volume on the heart, which ceases during microgravity. In addition, microgravity reduces the overall pressure load on the heart depending on the content of the countermeasure program. The mean arterial pressure slightly decreases. During spaceflight, the myocardial volume decreases by 8–10%.
3.4 Cardiovascular system after stabilization
After adaptation to microgravity, the cardiovascular system stabilizes, and the blood pressure is either unchanged or slightly lower [19]. Ambulatory blood pressure recording for 24 hours in eight astronauts revealed that the systolic, diastolic, and mean arterial pressures (mean ± se) in space were reduced by 8 ± 2 mmHg (p = 0.01; ANOVA), 9 ± 2 mmHg (P < 0.001), and 10 ± 3 mmHg (p = 0.006), respectively, with a maintained nocturnal dip of 8 ± 3 mmHg (p = 0.015). The cardiac stroke volume and output increased by 35 ± 10% and 41 ± 9% (p < 0.001), respectively, the heart rate and catecholamine concentrations were unchanged, and systemic vascular resistance was reduced by 39 ± 4% (p < 0.001).
3.5 Alteration of aerobic exercise capacity
Microgravity exposure reduces the circulatory blood volume; however, the maximal oxygen uptake is maintained after a short duration of spaceflight. During long-term spaceflight, the aerobic capacity decreases without countermeasures, but aerobic exercise training can maintain it, although standard exercise only markedly reduces the postflight maximal oxygen uptake. After a short duration of spaceflight (9–14 days), the maximal oxygen uptake decreased by 22%, probably due to decreases in the maximal stroke volume and maximal cardiac output without alterations in the maximal heart rate, blood pressure, or whole-body arteriovenous oxygen. This decrease in maximal oxygen uptake is believed to be due to the decreases in intravascular blood volume, stroke volume, and cardiac output.
As crew members are expected to work on the Moon/Martian surface, and they are exposed to extensive heat stress in the extravehicular suits, this aerobic capacity is considered to be significant after landing on the Moon/Mars.
3.6 Alterations in sympathetic neural traffic under microgravity
Sympathetic neural traffic indirectly measured by the plasma noradrenaline level has been reported to increase during spaceflight from the preflight control level [14, 20], and vagal activity estimated by power spectral analysis of heart rate variability was reduced after long-term spaceflight [21, 22].
Microneurographically recorded neural traffic in humans is known to be muscle and skin sympathetic nerve activity (MSNA and SSNA), and MSNA controls the vasomotor function of the muscular bed, responding to blood pressure changes against gravitational stress [23, 24, 25]. MSNA was suppressed during exposure to short-term microgravity induced by parabolic flight [26], mild lower body positive pressure (10–20-mmHg LBPP) [15], and thermoneutral head-out water immersion [27] responding to the loading or unloading of cardiopulmonary receptor-stimulated cephalad fluid shift. On the other hand, MSNA was increased after exposure to long-term microgravity in spaceflight and its simulation induced by dry immersion [28] or 6° head-down tilt bedrest [17] due to different mechanisms, including plasma volume loss, changes in baroreflex, and vascular compliance.
3.7 Postflight orthostatic intolerance
Orthostatic intolerance is usually observed after returning to 1 G on Earth. The definition of orthostatic intolerance usually includes simple syncope, lightheadedness, or >20-mmHg reduction in systolic blood pressure.
Astronauts usually notice orthostatic intolerance during prolonged upright standing rather than while standing up. Just before fainting, they sometimes have tachycardia, suggesting that they have postural orthostatic tachycardia syndrome (POTS). This phenomenon is due to a state in which fluid shift easily triggers tachycardia, which also easily triggers Bezold-Jarisch reflex, and the vagal response suppresses the systolic blood pressure. Although all astronauts stood upright for 10 min, 63% were unable to finish the stand test in 10 min.
Less important factors for postflight orthostatic intolerance are reduced compliance of the lower legs, reduced baroreflex sensitivity, and increased basal sympathetic tone.
Reduction of the circulatory blood volume is the most important factor for postflight orthostatic intolerance. The decrease in stroke volume after spaceflight reflects this circulatory blood volume loss. Although this is the main cause, the recovery of circulatory blood volume to the normal state is not complete. The crew members are recommended to take 8 g of salt and 1 L of water, which ameliorates the orthostatic tolerance, albeit not completely.
Another factor is the limitation by vasoconstriction. The postflight blood pressure of non-finishers cannot be increased by the total peripheral resistance compared with the preflight state. During the postflight upright standing 70° tilt test, the total peripheral resistance cannot increase despite activation of muscle sympathetic nerve activity, probably due to the alterations in venoarterial reflex and smooth muscle atrophy of the resistant vessels. Overall, circulatory blood volume reduction and attenuated vasoconstriction are the main factors for orthostatic intolerance.
3.8 Cardiovascular deconditioning
What is the cause of this cardiovascular deconditioning? NASA’s criteria of orthostatic intolerance are (1) presyncopal symptoms (pallor, cold sweat, nausea, blackout, and fainting), (2) gradual systolic blood pressure decrease <80 mmHg, (3) sudden systolic blood pressure decrease >15 mmHg, or (4) sudden heart rate decrease >15 bpm while on the 70° tilt bed for 15 min. A recent report stated that 65% of astronauts satisfied these criteria. Previously, this cardiovascular deconditioning was considered to be solely due to circulatory fluid loss, but other causes have also been explored.
In addition to the decrease in circulatory blood volume, other causes, i.e., altered arterial baroreflex gain, altered leg venous volume, easy fluid pooling in the space of atrophied skeletal muscles, attenuated muscle pump effects due to skeletal muscle atrophy, hypersensitivity of β-adrenergic receptors, and altered influence of vestibular (especially otolith) input, have been considered. Moreover, increased venous permeability of lower leg vessels and attenuated cardiopulmonary volume receptor reflex after −6° head-down tilt for 14 days were observed in our bedrest experiment. These changes are not the only cause of cardiovascular deconditioning, and multiple factors act in concert.
Several physiological and pathological neuro-ocular findings in astronauts/cosmonauts during and after long-term spaceflight, including hyperoptic shifts up to +1.75 diopters, optic disc edema (swelling), globe (eyeball) flattening, choroidal folds, and “cotton wool” spots in the fundus oculi, have been reported [29]. These findings have been documented as spaceflight-associated neuro-ocular syndrome. NASA has investigated the clinical, ultrasound, optical coherence tomography imaging, and fundus oculi findings of the above symptoms. In 2016, out of 47 or 64 astronauts examined, approximately 10 developed SANS (disc edema in 10/64, cotton wool spot in 7/64, choroidal folds in 11/47, globe flattening in 12/47, and refractive error in 9/47). It is unlikely that the duration of spaceflight is unrelated [30].
The exact cause of SANS has not been clarified, but its development is likely related to the increase in intracranial pressure due to the cephalad fluid shift. The increase in intracranial pressure is not necessarily due to microgravity exposure, but some percentage of astronauts had intracranial pressure change and developed SANS [29, 30].
Several countermeasures, e.g., lower body negative pressure, thigh cuffs, an impedance threshold device (ITD), vitamin B group administration, and artificial gravity, have been considered and are under trial. NASA and collaborating researchers continue to investigate SANS in preparation for future manned missions to space, including continued trips to the ISS, deep space gateway missions, a return to the Moon or Moon base, or a Martian expedition.
3.10 Brain structural plasticity during spaceflight
In 2016, structural changes in the brain during spaceflight were reported. Koppelmans et al. [31] evaluated retrospective longitudinal T2-weighted MRI scans and balance data from 27 astronauts (13, ~2-week Shuttle crew members, and 14, ~6-month ISS crew members) to assess spaceflight effects on brain structure. They observed extensive volumetric gray matter decreases, including large areas covering the temporal and frontal poles and around the orbits, and the effects were larger in ISS members than in Shuttle crew members. There were also bilateral focal gray matter increases within the medial primary somatosensory and motor cortex.
In 2017, a review on these MRI changes associated with spaceflight (actual or simulated) was reported. Van Ombergen et al. [32] discussed neuroplastic changes in the central nervous system and concluded that the cerebellum, cortical motor areas, and vestibular-related pathways are highly involved, demonstrating that these brain regions are indeed affected by actual and simulated spaceflight. Structural studies are now in progress, and functional relationships are under investigation. Long-term studies will be necessary to clarify the mechanism.
3.11 Effects of artificial gravity
We tested an intermittent short-arm centrifuge of 1.4 G with 60-W ergometric exercise with a step-up increase of 0.2 G and 15 W, respectively, for 30 min every day for 21 days during −6° head-down bedrest [33]. The circulatory blood volume was reduced by 20% in the control subjects, but no reduction was observed in the countermeasure subjects. Cardiac output and stroke volume were not changed in the countermeasure subjects, but they decreased in the control subjects. The baseline level of muscle sympathetic nerve activity (MSNA) was not changed in the countermeasure subjects, but it increased in the control subjects.
Therefore, everyday ergometric exercise under artificial gravity maintains the preflight cardiovascular state without adapting to microgravity.
4. Musculoskeletal system
4.1 Mechanism of muscle loss under microgravity
The first muscular measurements were performed in Skylab and Space Shuttle missions by the United States and in Salyut and Mir by the Soviet Union [34, 35, 36, 37]. The most prominent muscle loss was observed in the calf muscle (the soleus and gastrocnemius) after a few weeks in space. The muscle loss exhibited interindividual variation, but the maximum loss reached as high as 10%. This volume loss in the lower extremities accounts for most of the muscle atrophy and the blood and interstitial fluid shift. Although fluid shift away from the legs influences the size of these muscles, this phenomenon alone cannot explain the changes in leg volume on MRI. Muscle atrophy appears rapidly, usually between 8 and 11 days of flight, but can appear as early as the fifth day, as observed in one astronaut. Moreover, the effects of microgravity differ among muscles, with volume decreasing by 3.9% in the calf (the soleus and gastrocnemius) and 6% in the quadriceps femoris.
In addition to the morphological changes, functional alterations are associated with structural variations, and the muscular force is known to be reduced after spaceflight. In the Skylab 3 mission, it decreased by 20% after 53 days of microgravity exposure. Muscular electrical activity measured by electromyogram (EMG) had a lower EMG amplitude in addition to easy fatigability with a lower resistance.
The main cause of muscular loss is the disappearance of mechanical constraints and the subsequent decrease in muscular activity. The reduced muscular activity under microgravity is also associated with hypokinesia due to limited movement inside the spacecraft, which also can be observed in bedrest studies and animal experiments using tail suspension. The structural changes in skeletal muscle are also observed by microscopic examination under microgravity, which revealed that the proportion of type I red fibers decreased and they were replaced by type II white fibers. In 1995, pre- and postflight human muscle biopsies were performed on three and five astronauts during 5- and 11-day missions, respectively. In this study, the muscle fiber diameter decreased by 15 to 30%, and the number of capillaries around the muscle fibers decreased. The proportion of type I fibers changed from 43 (preflight) to 37% (postflight) after 5-day missions, and that of type II fibers changed from 57 to 67%. After 11 days of spaceflight, the proportion of type I fibers decreased from 45 to 39%, and that of type II fibers decreased from 55 to 61%, consistent with the animal experiments that demonstrated that gravity can influence genes regulating the protein synthesis of muscle protein degradation enzymes.
These changes were confirmed to be due to both an increase in protein breakdown and decrease in synthesis. Human biochemical examination also revealed a higher level of muscle protein degradation, increased level of urinary amino acids, and higher level of creatinine. The diet of astronauts is protein-rich, but the degradation process is such that nitrogen losses overcome the gains and the nitrogen balance becomes negative.
Recent studies have suggested the mechanism of disuse atrophy of the skeletal muscle, especially oxidative stress, to be an important regulator of pathways leading to muscle atrophy during periods of disuse. Redox disturbances, such as those in skeletal muscle myotubes, increase the expression of key components of the proteasome proteolytic system, which is a prominent factor in protein degradation in disused muscles.
Another hypothesized mechanism is the degradation of muscle proteins resulting from their ubiquitination. These molecular mechanisms underlie protein degradation during disuse.
4.2 Countermeasures for muscle loss
In order to prevent muscle loss, several countermeasures were available during microgravity exposure in Shuttle missions and continue to be available on the ISS. These include aerobic exercise, stretching, strength training, and electrical stimulation. Artificial gravity with exercise has been proposed as a potential measure for muscle loss because ground-based studies confirmed it to be effective, but a short-arm centrifuge has not been mounted. In addition to physical stimulation, medications, such as antioxidants, growth hormone, growth factors, ubiquitin, clenbuterol, anabolic steroids, and amino acids, are candidates against muscle loss.
Aerobic exercise is the most effective countermeasure for maintaining the fast twitch red fibers. On the ISS, the combination of an ergometer, treadmill, and the Advanced Resistive Exercise Device (ARED) is ideal to maintain muscle power and the morphology of antigravity muscles (empowerment of both fast and slow twitch fiber muscles).
Stretching can minimize atrophy by maintaining the muscle as much as possible in the stretched condition. In the Russian space program, the penguin suit—a snug fitting, full-length, long sleeved jumpsuit made with elastic inserts at the collar, waist, wrists, and ankles and along the vertical sides of the suit—loads the body along the long axis with an adjustable force of 15–40 kg, while the other elastic elements make it possible to adjust the position of the limbs. The angle of the major joints, such as the knee and ankle, can be set, allowing the foot to be dorsiflexed, which will stretch the soleus. The effects of stretching are not well understood, but it is a valid countermeasure considering human physiology.
Strength training by resistance exercise is also employed as a countermeasure for muscle loss. Weight training studies recommended a good mix of exercise types to be 15% (eccentric), 10% (isometric), and 75% (concentric weight-bearing). The most recommended exercise for resistance training is squatting.
Electric stimulation is also expected to increase protein synthesis and prevent the decrease in oxidative enzymes inducing disuse atrophy.
4.3 Artificial gravity with exercise
We previously confirmed the effectiveness of artificial gravity in bedrest studies [33]. Our results demonstrated that artificial gravity of 1.4 G with ergometric exercise maintains the muscle strength and cross-sectional area of the quadriceps femoris measured by MRI. Another study revealed that artificial gravity with squatting exercise also maintains the function and morphology of the soleus and gastrocnemius [38].
5. Bone metabolism system
The main problem of the skeletal system is bone calcium (Ca2+) loss during microgravity. The bone becomes fragile during microgravity exposure, which can harm an astronaut or cosmonaut even after returning to Earth. Moreover, the risk of renal stones is high during long-term missions due to hypercalcemia [39].
Ca2+ plays an essential role in bone structure, contraction of skeletal and cardiac muscles, neural transmission, blood coagulation, cell permeability, and hormonal signaling. The serum Ca2+ level is well maintained at 8.4–10.2 mg/dL. Ca2+ is absorbed from the small intestine (300 mg/day), into the blood, deposited in the bone (500 mg/day), and excreted from the kidneys (150 mg/day) or into feces.
In this section, the influences of gravity on bone structure and of hormones on bone formation and absorption are described.
5.1 Bone development and restructuring
Gravity influences the long bones of the lower extremities, e.g., the femur, tibia, calcaneus, and vertebrae, which support the body in the upright position. Bone tissue contains osteocytes, which develop from osteoblasts, and are changed into osteoclasts by the action of RANKL (also called osteoclast differentiation factor, short for receptor activation of NF-kappa B ligand).
Osteoblasts and osteoclasts are functionally closely related, as is the balance between bone formation and bone resorption. Thus, insufficient bone formation compared with bone resorption observed in spaceflight reduces the bone mass and bone strength, leading to fractures.
Two hormones, calcitonin and parathormone (PTH), and vitamin D play an essential role in Ca2+ metabolism. Calcitonin is secreted from C cells of the thyroid gland. The secretion of calcitonin is promoted by an increase in the blood calcium concentration and is suppressed by the decrease in the serum calcium level. Calcitonin acts on the calcitonin receptor in osteoclasts to suppress the release of Ca2+ from the bone and promotes the deposition of calcium and phosphate on the bone. Calcitonin also promotes the excretion of calcium and phosphate into the urine. As a result, the serum level of Ca2+ decreases.
PTH is secreted from the parathyroid gland, increasing the release of Ca2+ from bone. PTH binds to osteoblasts to increase the expression of RANKL and inhibits their secretion of osteoprotegerin (OPG), which competitively binds to RANKL, preventing RANKL from interacting with RANK (receptor for RANKL). The binding of RANKL stimulates osteoclast precursors to fuse, forming new osteoclasts. As a result, PTH increases bone resorption, thereby increasing the serum Ca2+ level.
Vitamin D (25-hydroxycholecalciferol) acts on the parathyroid gland and suppresses the synthesis and secretion of PTH. The intestinal tract promotes the absorption of calcium and phosphorus. Vitamin D is essential for bone formation, but its direct action on bone formation remains unclear. It is also necessary for the formation of osteoclasts, affects the bone action of PTH, and promotes bone resorption itself at a high concentration. In the kidney, vitamin D increases Ca2+ reabsorption in the distal tubule and promotes the Ca2+ reabsorption action of PTH.
5.2 Effects of microgravity on bone metabolism
The main factor of bone metabolism is mechanical impact. Gravity creates weight and is responsible for the pressure exerted on a large part of the skeleton, resulting in a mechanical impact on bones. These gravitational impacts provide mechanical constraints on the femurs, tibias, calcaneus, and vertebrae. Thus, decalcification and bone loss are observed as the result of bone resorption, and the disappearance of gravity from the body axis components induces bone loss and resultant osteoporosis [2, 40].
5.3 Effects of spaceflight on bone metabolism
In microgravity conditions, decalcification was observed in 12 of the astronauts on the Gemini and Apollo 7 and 8 flights in 1969 [8]. Based on bone density measured using X-rays, the bone Ca2+ loss was 3.2%.
The bone mineral density was measured before and after the Mir program. The changes were as follows: +0.6% in the skull, +0.1% in the arm, −1.07% in the spine, −1.35% in the pelvis, −1.16% in the femoral neck, −1.58% in the trochanter major, −1.25% in the tibia, and −1.50% in the calcaneus per month, with comparable results from the ISS [41]. The most affected bones during spaceflight are weight-bearing bones, e.g., the pelvis (os coxae), the trochanter major of the femur, the femoral neck, the tibia, and the calcaneus.
Mir studies using dual photonic densitometry demonstrated a mean decrease in bone mineral density of approximately 0.3%/month in the cortical bone and up to 0.9%/month in cancellous tibial bone. Decalcification only occurs in the weight-bearing bones, and demineralization is correlated with mission duration. During spaceflight, hypercalcemia and hyperphosphatemia develop due to demineralization, and Ca2+ excretion into the urine increases before stabilization at around the 30th day of flight [42].
The National Aeronautics and Space Administration (NASA) of the United States documented a bone mineral loss rate/month of 1–2% during spaceflight (https://science.nasa.gov/science-news/science-at-nasa/2001/ast01oct_1), and bone density loss of 5–6% was reported in Apollo 15 crewmembers [43]. Bone loss is influenced by the spaceflight duration.
Tail suspension studies on rats demonstrated that simulated microgravity reduces bone formation, alters the Ca2+ balance, and inhibits the proliferation and differentiation of osteoprogenitor cells [44]. Osteocytes can also be affected by unloading stimulus in a bioreactor, with high expression of inhibitors of bone formation (sclerotin) and stimulators of bone resorption (RANKL) [45].
Osteoporosis can be irreversible. After returning to Earth without appropriate rehabilitation, the bone may be unable to return to normal activity under loads and may be weaker, easily inducing fractures. Reloading after a period of a week can ameliorate bone weakness, but even 2 weeks of bone restoration was not satisfactory. The length of spaceflight influences the bone density loss; however, another report stated that the bone loss at 1 month continued to increase after 6 months, suggesting that the length of spaceflight does not determine the bone density loss [42].
5.4 Effects of mechanical impact on hormonal influence
Wolff’s law characterizes how the bone adapts to functionally withstand its mechanical environment [46]; however, several studies found that mechanical loading per se is not the direct stimulus for bone remodeling [47, 48, 49, 50, 51].
Then what are the effects of mechanical impact on calcitonin? Calcitonin receptors were not observed on osteoblasts [52] but were present on osteoclasts [53] and osteocytes [54]. Calcitonin was reported to inhibit apoptosis of osteoblasts and osteocytes, demonstrating a potential indirect influence on bone formation. These data confirmed that mechanical impact is not directly related to bone formation.
One notable property of PTH is that although chronic increases in PTH levels increase bone resorption, intermittent stimulation accelerates bone formation. PTH stimulates osteoclast formation by binding to PTH receptor 1 on stromal/osteoblastic cells and thereby increases the production of receptor activator of RANKL and macrophage colony-stimulating factor (M-CSF) and suppresses the RANKL decoy receptor osteoprotegerin. Moreover, PTH controls the production of osteoblasts through actions on osteocytes through Wnt signaling in osteoblastogenesis [55].
The action of osteocytes, which can directly sense a mechanical unloading stimulus, increased the expression of both inhibitors of bone formation (SOST/sclerotin) and stimulators of bone resorption (RANKL) through Wnt signaling [45]. These results support the hypothesis that intermittent mechanical impacts induce osteocyte action, which inhibits bone formation and stimulates bone resorption, and that an intermittent increase in PTH controls the production of osteoblasts.
5.5 Sympathetic alteration of bone metabolism during spaceflight
It has been reported that sympathetic neural traffic to bone inhibits the function of osteoblast and increases that of osteoclast, thus facilitating bone loss. Possible roles of the sympathetic nervous system in the mechanisms of bone loss in humans exposed to long-term spaceflight will be discussed.
Prolonged exposure to microgravity in space for 14 days increased sympathetic neural traffic in humans based on results from the Neurolab mission [14, 56, 57, 58], with comparable increases in noradrenaline spillover and clearance in space [14]. Concordant results were obtained during simulated microgravity, including dry immersion [28] or head-down bedrest [17]. In general, elderly people have a low bone density and high sympathetic neural traffic to muscles [59]. Our preliminary study demonstrated that changes in sympathetic neural traffic to muscles after long-term bedrest of 20 days were significantly correlated with changes in the urinary secretion level of deoxypyridinoline [25, 60], which is used as a specific marker of bone resorption [61]. Based on these findings, exposure to prolonged microgravity may increase sympathetic neural traffic to the bone, which increases the noradrenaline level, thereby inhibiting osteogenesis and facilitating osteolysis through β-receptors to induce bone mineral loss.
5.6 Countermeasures for space-related osteoporosis
Physical factors
Exercise during weightlessness has been incorporated into the present countermeasure programs; however, exercise alone cannot prevent bone loss. The current exercise program for the ISS is a combination of aerobic and resistive exercise for 2.5 hours, 6 days/week. Data from spaceflight revealed that bone loss occurs mainly in the femur, tibia, calcaneus, and vertebrae. Therefore, exercise should be concentrated on these bones, and impact loading should be primarily provided rather than static loading [62].
Pharmacological factors
As bone mass is sufficient at the onset of the spaceflight, the optimal strategy for the pharmacotherapy against bone loss is the prevention of bone loss, not the acceleration of bone formation, when loading is removed during spaceflight. Several drugs have been proposed to prevent bone loss under microgravity.
Bisphosphonates
Bisphosphonates have two phosphonate (PO3) groups and are similar in structure to pyrophosphate. They bind to hydroxyapatite in bone matrix and prevent bone loss by inhibiting osteoclastic bone resorption. Bisphosphonates have been demonstrated to be effective in preventing bone loss during bedrest studies [63, 64, 65, 66]. Among several types of bisphosphonates, pamidronate has been confirmed to suppress bone mineral loss and to prevent the formation of renal stones during bedrest studies [67].
In 2010, LeBlanc and Matsumoto [68] proposed an experiment for the effectiveness of bisphosphonate as a countermeasure to spaceflight-induced bone loss. The astronauts chose either oral administration of alendronate at 70 mg once per week or intravenous administration of zoledronate at 4 mg before the flight, and their bone densities were examined by DXA, QCT, and pQCT, and bone metabolism markers, including bone formation and resorption markers, and renal stone formation were assessed. One of the co-investigators (Ohshima) reported successful suppression of spaceflight-induced bone loss and renal stone formation (Ohshima, personal communication).
The disadvantages of bisphosphonates are local irritation of the upper gastrointestinal (GI) tract and poor absorption from the GI tract. Therefore, the oral administration of bisphosphonates requires drinking 200 mL of water while remaining in an upright posture for at least 30 min until after their first meal of the day to facilitate delivery to the stomach. This poses a problem as there is no upright posture in space due to microgravity. Another potential problem is osteonecrosis of the maxilla and the mandible, although the incidence is low [69]. These osteonecrotic or osteolytic phenomena always accompany physiological stress (mastication), iatrogenic trauma (tooth extraction/denture injury), or tooth infection [70, 71].
Bisphosphonates are difficult to metabolize, and high concentrations of them are maintained in the bones for long periods. As bone formation is closely coupled with bone turnover, long-term use of the compound with resultant suppression of bone turnover can compromise healing of even physiological microinjuries within the bone. Osteonecrosis of the maxilla and mandible likely results from the inability of the hypodynamic and hypovascular bone to meet the increased demand for repair and remodeling because several alterations are associated with this necrosis.
Parathormone
Parathormone has anabolic effects on the bone and also functions in the kidney to stimulate the reabsorption of Ca2+ and increase the synthesis of vitamin D. In this sense, parathormone may stimulate bone formation, increase vitamin D synthesis, and stimulate Ca2+ reabsorption. As suppressing bone reabsorption is favorable for stimulating bone formation during spaceflight, the administration of parathormone is strategically unfavorable.
In conclusion, it is favorable to administer bisphosphonate orally under artificial gravity with exercise in order to prevent osteoporosis in space. Monitoring the blood and urine samples on the ISS or spacecraft by a simple method is necessary to assess the effectiveness of the countermeasure.
6. Immunology and hematology
6.1 Space anemia
The circulatory blood volume is 5 L on average and contains plasma and cellular components, including erythrocytes, leukocytes (neutrophils, eosinophils, basophils, and lymphocytes), and platelets [72, 73, 74]. Among them, reduction in cellular components, especially erythrocytes (RBC), is associated with anemia, whereas the function of leukocytes is related to immunological response.
In the early stages of space development, cases of “space anemia” (hematocrit reduction) were reported on Gemini, Apollo, Skylab, and Shuttle missions and in the cosmonauts in the Salyut and Mir missions. However, in spaceflight, microgravity causes cephalad fluid shift, meaning this “space anemia” was actually a misinterpretation of symptoms. The true effects of microgravity can be measured through the total RBC count calculated from the hematocrit and plasma volume measurements. In this way, “space anemia” corresponded to a reduction in the total RBC count.
After 10 days aboard Spacelab-1, the total RBC count was reduced by 9% and by 15% after several weeks. After returning to Earth, the total RBC count did not recover even after 6 weeks and, in the case of Skylab astronauts, had not recovered after more than 3 months.
This suggested that microgravity is responsible for “space anemia,” and many investigations were carried out to reveal whether anemia is the result of an increase in RBC destruction or a decrease in their production. Using labeled RBC by the uptake of 14C glycine, RBC destruction was found to be three times greater in rats having flown aboard Cosmos-782 than in the control rats. On the other hand, reduced RBC production is unlikely because the number of stem cells measured by the number of cellular colonies that developed in vitro from samples of bone marrow taken from rats that flew aboard the Soviet Biosatellite—2044 for 14 days—was unchanged.
Human studies carried out by [75] on Shuttle missions for 9 to 14 days demonstrated that space anemia is due mainly to a lower production of RBC, causing increased plasma volume, reduced hemoglobin concentration, and increased serum erythropoietin. This reflects a decrease in the RBC life span and slower production.
Rizzo et al. [76] analyzed the cause of the shortened RBC life span and reported altered cell membrane composition and an increase in lipid peroxidation products. They suggested that antioxidant defense systems in the erythrocytes were induced, with a significant increase in glutathione content.
The mechanism underlying anemia was also confirmed by measuring the erythropoietin (EPO) level [77]. Radioimmunoassay revealed that the EPO level decreases after 24 hours of flight and is reduced by 30–40% on the third day compared with preflight levels. This low secretion of EPO will inhibit RBC maturation and cause hemolysis due to suppressed erythropoiesis.
Other changes in leukocytes (WBC) are in their polymorphonuclear characteristics. The composition of WBC is changed such that there is a slight increase in neutrophils and decrease in eosinophils. The percentage of lymphocytes, especially T cells, decreases, whereas that of monocytes slightly increases. These changes quickly disappear upon returning to 1 G on Earth.
6.2 Immunological changes during weightlessness
Recent studies confirmed dysregulation of the immunological response in humans and the reactivation of latent herpes virus, which persisted for the duration of a 6-month orbital spaceflight [78]. Blood samples from ISS crew members demonstrated that long exposure to microgravity reduced their T lymphocyte counts, suggesting the attenuation of cytotoxic function and viral reactivation in the space environment.
As the immune system is highly sensitive to different types of stressors, including psychological, physical, and local environmental stressors (e.g., oxidative and radiation exposure), exposure to the space environment suppresses T helper cells, which leads to susceptibility to viruses.
7. Artificial gravity as a total countermeasure for spaceflight deconditioning
For human space voyages lasting several years, such as those envisioned for the exploration of Mars, astronauts will be at risk of catastrophic consequences should any of the systems that provide air, water, food, or thermal protection fail. Beyond that, astronauts will face serious health and/or safety risks resulting from marked physiological deconditioning associated with prolonged weightlessness [1, 79]. The principal physiological deconditioning risks are related to physical and functional deterioration, and the loss of regulation of the several systems, including blood circulation, decreased aerobic capacity, musculoskeletal systems, and altered sensorimotor system performance. These physiological effects of weightlessness are generally adaptive to spaceflight and present a hazard only following G transitions upon returning to Earth or landing on another planet [80]. Among them, bone mineral metabolism will be greatly affected during prolonged spaceflight.
7.1 Why artificial gravity
Space biomedical researchers have been working for many years to develop “countermeasures” to reduce or eliminate the deconditioning associated with prolonged weightlessness. Intensive and sustained aerobic exercise on a treadmill, bicycle, or rowing machine coupled with intensive resistive exercise has been used on US and Russian spacecraft to minimize these problems. The procedures were uncomfortable and excessively time-consuming for many astronauts, and their effectiveness for maintaining bone, muscle, and aerobic fitness has not been demonstrated due in part to the low reliability of the devices flown to date. Furthermore, they have had inconsistent effects on postflight orthostatic hypotension or sensorimotor adaptive changes. With the exception of fluid loading before reentry, other countermeasures (e.g., diet, lower body negative pressure, or wearing a “penguin suit” to force joint extension against a resistive force) either have been marginally effective or presented an inconvenience or hazard.
To succeed in the near-term goal of a human mission to Mars during the second quarter of this century, the human risks associated with prolonged weightlessness must be mitigated well beyond our current capabilities. Indeed, during nearly 45 years of human spaceflight experience, including numerous long-duration missions, no single countermeasure or combination of countermeasures that is completely effective has been developed. Current operational countermeasures have not been rigorously validated and have not fully protected any long-duration (>3 months) astronauts in low Earth orbit. Thus, it is unlikely that they will sufficiently protect astronauts journeying to Mars and back over a 3-year period.
Although improvements in exercise protocols, changes in diet, or pharmaceutical treatments of individual systems may be of value, they are unlikely to eliminate the full range of physiological deconditioning. Therefore, a complete research and development program aimed at substituting the missing gravitational cues, and loading in space is warranted.
The urgency of exploration-class countermeasures is compounded by the limited availability of flight resources for validating a large number of system-specific countermeasure approaches. Furthermore, recent evidence of the rapid degradation of pharmaceuticals flown aboard long-duration missions, putatively because of radiation effects, raises concerns regarding the viability of some promising countermeasure development results. Although the rotation of a Mars-bound spacecraft will not be a panacea for all human risks of spaceflight (artificial gravity cannot solve the problems associated with radiation exposure, isolation, confinement, and environmental homeostasis), artificial gravity does offer significant promise as an effective, efficient, multi-system countermeasure against the physiological deconditioning associated with prolonged weightlessness. Virtually all of the identified risks associated with cardiovascular deconditioning, myatrophy, bone loss, neurovestibular disturbances, space anemia, immune compromise, and neurovegetative state may be alleviated by sufficient artificial gravity.
7.2 Why artificial gravity with exercise
Although a short-radius centrifuge has been proposed several times, loading with artificial gravity has not been demonstrated to be effective at preventing spaceflight deconditioning on its own. Making a human-powered short-arm centrifuge is an effective method to create exercise loads for astronauts. Considering the size of the ISS, it is appropriate to employ a short-radius centrifuge rather than a large-radius human centrifuge; however, it may be beneficial to rotate the spacecraft itself to provide the artificial gravity for long-duration spaceflight such as Mars expeditions.
In 1999, Iwase proposed the creation of artificial gravity by ergometric exercise, and it was installed at Nagoya University [33]. Several studies were performed using this short-radius centrifuge with an ergometer. In 2002, a bedrest study was carried out to evaluate the effectiveness of artificial gravity with ergometric exercise. In 2005, the facility was moved to Aichi Medical University, and bedrest studies were performed to finalize the protocol. This daily AG-EX step-up protocol was confirmed to be effective at preventing cardiovascular, musculoskeletal, and bone metabolism deconditioning in 2006, whereas the alternate-day (every-other-day) protocol (loading the AG-EX every other day) did not improve the spaceflight deconditioning associated with the microgravity exposure analogue of −6° head-down bedrest.
The authors applied for the installation of a short-radius centrifuge facility on the ISS and proposed it as a method to prevent spaceflight deconditioning, including bone loss. This project, Artificial Gravity with Ergometric Exercise (AGREE project), was promising to prevent space deconditioning during spaceflight, but it was canceled halfway through (Figure 1).
Figure 1.
Structure of the device of artificial gravity with exercise for AGREE project 2012.
8. Conclusion and summary
Several deconditioning states in the neurovestibular, cardiovascular, ocular, musculoskeletal, bone metabolic, hematological and immunological, and central nervous systems have been documented, and efforts to ameliorate the symptoms have been made. In the near future, space medicine will play an increasingly important role in missions to the Moon and Martian expeditions as well as in future deep space exploration.
Historically, space medicine examined early adaptation to microgravity and early readaptation to the terrestrial 1 G state. However, the philosophy of the authors is to avoid adaptation to microgravity using artificial gravity. Under this scenario, short exposure to microgravity is permitted, but longer adaptation will be unnecessary. With this philosophy, the authors believe that the humans will achieve safe and comfortable spaceflight without deconditioning.
\n',keywords:"microgravity, neurovestibular, neural plasticity, cardiovascular, musculoskeletal, bone metabolism, hematology and immunology",chapterPDFUrl:"https://cdn.intechopen.com/pdfs/70679.pdf",chapterXML:"https://mts.intechopen.com/source/xml/70679.xml",downloadPdfUrl:"/chapter/pdf-download/70679",previewPdfUrl:"/chapter/pdf-preview/70679",totalDownloads:1387,totalViews:0,totalCrossrefCites:7,dateSubmitted:"May 17th 2019",dateReviewed:"November 29th 2019",datePrePublished:"February 5th 2020",datePublished:"May 27th 2020",dateFinished:"December 30th 2019",readingETA:"0",abstract:"The effects of microgravity conditions on neurovestibular, cardiovascular, musculoskeletal, bone metabolic, and hemato-immunological systems are described. We discuss “space motion sickness,” sensorimotor coordination disorders, cardiovascular deconditioning, muscular atrophy, bone loss, and anemia/immunodeficiency, including their causes and mechanisms. In addition to the previously described deconditioning, new problems related to microgravity, spaceflight-associated neuro-ocular syndrome (SANS), and structural changes of the brain by magnetic resonance imaging (MRI) are also explained. Our proposed countermeasure, artificial gravity produced by a short-arm centrifuge with ergometric exercise, is also described in detail, and we confirmed this system to be effective in preventing the abovementioned deconditioning caused by microgravity exposure.",reviewType:"peer-reviewed",bibtexUrl:"/chapter/bibtex/70679",risUrl:"/chapter/ris/70679",signatures:"Satoshi Iwase, Naoki Nishimura, Kunihiko Tanaka and Tadaaki Mano",book:{id:"7632",type:"book",title:"Beyond LEO",subtitle:"Human Health Issues for Deep Space Exploration",fullTitle:"Beyond LEO - Human Health Issues for Deep Space Exploration",slug:"beyond-leo-human-health-issues-for-deep-space-exploration",publishedDate:"May 27th 2020",bookSignature:"Robert J. Reynolds",coverURL:"https://cdn.intechopen.com/books/images_new/7632.jpg",licenceType:"CC BY 3.0",editedByType:"Edited by",isbn:"978-1-78985-510-4",printIsbn:"978-1-78985-509-8",pdfIsbn:"978-1-83880-849-5",isAvailableForWebshopOrdering:!0,editors:[{id:"220737",title:"Dr.",name:"Robert",middleName:null,surname:"J. Reynolds",slug:"robert-j.-reynolds",fullName:"Robert J. Reynolds"}],productType:{id:"1",title:"Edited Volume",chapterContentType:"chapter",authoredCaption:"Edited by"}},authors:[{id:"76278",title:"Prof.",name:"Satoshi",middleName:null,surname:"Iwase",fullName:"Satoshi Iwase",slug:"satoshi-iwase",email:"s_iwase@nifty.com",position:null,profilePictureURL:"//cdnintech.com/web/frontend/www/assets/author.svg",institution:{name:"Aichi Medical University",institutionURL:null,country:{name:"Japan"}}},{id:"321445",title:"Dr.",name:"Naoki",middleName:null,surname:"Nishimura",fullName:"Naoki Nishimura",slug:"naoki-nishimura",email:"guhergpin@gmail.com",position:null,profilePictureURL:"//cdnintech.com/web/frontend/www/assets/author.svg",institution:null},{id:"321447",title:"Dr.",name:"Kunihiko",middleName:null,surname:"Tanaka",fullName:"Kunihiko Tanaka",slug:"kunihiko-tanaka",email:"4z9ztrwhw9rhwe@gmail.com",position:null,profilePictureURL:"//cdnintech.com/web/frontend/www/assets/author.svg",institution:null},{id:"321448",title:"Dr.",name:"Tadaaki",middleName:null,surname:"Mano",fullName:"Tadaaki Mano",slug:"tadaaki-mano",email:"mano197814t75tn2f@gmail.com",position:null,profilePictureURL:"//cdnintech.com/web/frontend/www/assets/author.svg",institution:null}],sections:[{id:"sec_1",title:"1. Introduction",level:"1"},{id:"sec_2",title:"2. Neurovestibular system",level:"1"},{id:"sec_2_2",title:"2.1 Space motion sickness",level:"2"},{id:"sec_3_2",title:"2.2 Countermeasures for space motion sickness",level:"2"},{id:"sec_5",title:"3. Cardiovascular system",level:"1"},{id:"sec_5_2",title:"3.1 Effects of microgravity in the cardiovascular system",level:"2"},{id:"sec_6_2",title:"3.2 Decrease in the circulatory blood volume",level:"2"},{id:"sec_7_2",title:"3.3 Reduced heart size",level:"2"},{id:"sec_8_2",title:"3.4 Cardiovascular system after stabilization",level:"2"},{id:"sec_9_2",title:"3.5 Alteration of aerobic exercise capacity",level:"2"},{id:"sec_10_2",title:"3.6 Alterations in sympathetic neural traffic under microgravity",level:"2"},{id:"sec_11_2",title:"3.7 Postflight orthostatic intolerance",level:"2"},{id:"sec_12_2",title:"3.8 Cardiovascular deconditioning",level:"2"},{id:"sec_13_2",title:"3.9 Spaceflight-associated neuro-ocular syndrome (SANS)",level:"2"},{id:"sec_14_2",title:"3.10 Brain structural plasticity during spaceflight",level:"2"},{id:"sec_15_2",title:"3.11 Effects of artificial gravity",level:"2"},{id:"sec_17",title:"4. Musculoskeletal system",level:"1"},{id:"sec_17_2",title:"4.1 Mechanism of muscle loss under microgravity",level:"2"},{id:"sec_18_2",title:"4.2 Countermeasures for muscle loss",level:"2"},{id:"sec_19_2",title:"4.3 Artificial gravity with exercise",level:"2"},{id:"sec_21",title:"5. Bone metabolism system",level:"1"},{id:"sec_21_2",title:"5.1 Bone development and restructuring",level:"2"},{id:"sec_22_2",title:"5.2 Effects of microgravity on bone metabolism",level:"2"},{id:"sec_23_2",title:"5.3 Effects of spaceflight on bone metabolism",level:"2"},{id:"sec_24_2",title:"5.4 Effects of mechanical impact on hormonal influence",level:"2"},{id:"sec_25_2",title:"5.5 Sympathetic alteration of bone metabolism during spaceflight",level:"2"},{id:"sec_26_2",title:"5.6 Countermeasures for space-related osteoporosis",level:"2"},{id:"sec_28",title:"6. Immunology and hematology",level:"1"},{id:"sec_28_2",title:"6.1 Space anemia",level:"2"},{id:"sec_29_2",title:"6.2 Immunological changes during weightlessness",level:"2"},{id:"sec_31",title:"7. Artificial gravity as a total countermeasure for spaceflight deconditioning",level:"1"},{id:"sec_31_2",title:"7.1 Why artificial gravity",level:"2"},{id:"sec_32_2",title:"7.2 Why artificial gravity with exercise",level:"2"},{id:"sec_34",title:"8. Conclusion and summary",level:"1"}],chapterReferences:[{id:"B1",body:'Buckey JC Jr. Preparing for Mars: The physiologic and medical challenges. European Journal of Medical Research. 1999;4:353-356'},{id:"B2",body:'Buckey JC Jr. Space Physiology. New York: Oxford University Press; 2006. pp. 1-283'},{id:"B3",body:'Clément G. Fundamentals of Space Medicine. 2nd ed. New York: Springer; 2011. pp. 1-381'},{id:"B4",body:'International Academy of Astronautics Study Group, editor. Bone standard measures. In: International Academy of Astronautics Study Group. 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The Journal of Physiology. 2002;538:321-329'},{id:"B15",body:'Fu Q, Sugiyama Y, Kamiya A, Shamsuzzaman ASM, Mano T. Responses of muscle sympathetic nerve activity to lower body positive pressure. The American Journal of Physiology. 1998;275:H1254-H1259'},{id:"B16",body:'Grigoriev AI, Morukov BV, Vorobiev DV. Water and electrolyte studies during long-term missions onboard the space stations SALYUT and MIR. The Clinical Investigator. 1994;72:169-189'},{id:"B17",body:'Kamiya A, Iwase S, Kitazawa H, Mano T, Vinogradova OL, Kharchenko IB. Baroreflex control of muscle sympathetic nerve activity after 120 days of 6 degrees head-down bed rest. American Journal of Physiology. Regulatory, Integrative and Comparative Physiology. 2000;278:R445-R452'},{id:"B18",body:'Diedrich A, Paranjape SY, Robertson D. Plasma and blood volume in space. The American Journal of the Medical Sciences. 2007;334:80-85'},{id:"B19",body:'Norsk P, Asmar A, Damgaard M, Christensen NJ. 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Aminohydroxybutane bisphosphonate inhibits bone loss due to immobilization in rats. Journal of Bone and Mineral Research. 1990;5:279-286'},{id:"B66",body:'LeBlanc A, Shackelford L, Schneider V. Future human bone research in space. Bone. 1998;22(5 Suppl):113S-116S'},{id:"B67",body:'Watanabe Y, Ohshima H, Mizuno K, Sekiguchi C, Fukunaga M, Kohri K, et al. Intravenous pamidronate prevents femoral bone loss and renal stone formation during 90-day bed rest. Journal of Bone and Mineral Research. 2004;19:1771-1778'},{id:"B68",body:'LeBlanc A, Matsumoto T, Jones J, Shapiro J, Lang T, Smith SM, et al. Bisphosphonate as a countermeasure to space flight-induced bone loss. 2010. Available from: http://www.dsls.usra.edu/meetings/hrp2010/pdf/Bone/1094LeBlanc.pdf'},{id:"B69",body:'Durie BGM, Katz M, Crowley J. Osteonecrosis of the jaw and bisphosphonates. The New England Journal of Medicine. 2005;353:99-102'},{id:"B70",body:'Ruggiero SL, Mehrotra B, Rosenberg TJ, Engroff SL. Osteonecrosis of the jaws associated with the use of bisphosphonates: A review of 63 cases. Journal of Oral and Maxillofacial Surgery. 2004;62:527-534'},{id:"B71",body:'Ruggiero SL, Woo SB. Biophosphonate-related osteonecrosis of the jaws. Dental Clinics of North America. 2008;52:111-128'},{id:"B72",body:'De Santo NG, Cirillo M, Kirsch KA, Correale G, Drummer C, Frassl W, et al. Anemia and erythropoietin in space flights. Seminars in Nephrology. 2005;25:379-387'},{id:"B73",body:'Kunz H, Quiriarte H, Simpson BJ, Ploutz-Snyder R, McMonigal K, Sams C, et al. Alterations in hematologic indices during long-duration spaceflight. BMC Hematology. 2017;17:12-19'},{id:"B74",body:'Smith SM. Red blood cell and iron metabolism during space flight. Nutrition. 2002;18:864-866'},{id:"B75",body:'Alfrey CP, Udden MM, Leach-Huntoon C, Driscoll T, Pickett MH. Control of red blood cell mass in spaceflight. Journal of Applied Physiology. 1996;81:98-104'},{id:"B76",body:'Rizzo AM, Corsetto PA, Montorfano G, Milani S, Zava S, Tavella S, et al. Effects of long-term space flight on erythrocytes and oxidative stress of rodents. PLoS One. 2012;7(3):e32361'},{id:"B77",body:'Gunga H-C, Kirsch K, Baartz F, Maillet A, Gharib C, Nalishiti W, et al. Erythropoietin under real and simulated microgravity conditions in humans. Journal of Applied Physiology. 1996;81:761-773'},{id:"B78",body:'Crucian BE, Chouker A, Simpson R, Mehta S, Marshall G, Smith SM, et al. Immune system dysregulation during spaceflight: Potential countermeasures for deep space exploration missions. Frontiers in Immunology. 2018;9:1437. DOI: 10.3389/fimmu.2018.01437'},{id:"B79",body:'Clément G, Bukley A, editors. Artificial Gravity. Hawthorne, CA and New York, NY: Microcosm Press and Springer; 2007. pp. 1-364'},{id:"B80",body:'Young LR. Artificial gravity considerations for a Mars exploration mission. 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IntechOpen’s Academic Editors and Authors have received funding for their work through many well-known funders, including: the European Commission, Bill and Melinda Gates Foundation, Wellcome Trust, Chinese Academy of Sciences, Natural Science Foundation of China (NSFC), CGIAR Consortium of International Agricultural Research Centers, National Institute of Health (NIH), National Science Foundation (NSF), National Aeronautics and Space Administration (NASA), National Institute of Standards and Technology (NIST), German Research Foundation (DFG), Research Councils United Kingdom (RCUK), Oswaldo Cruz Foundation, Austrian Science Fund (FWF), Foundation for Science and Technology (FCT), Australian Research Council (ARC).
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If you are associated with any of the institutions in our list below, you can apply to receive OA publication funds by following the instructions provided in the links. Please consult the Open Access policies or grant Terms and Conditions of any institution with which you are linked to explore ways to cover your publication costs (also accessible by clicking on the link in their title).
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Open Access publication costs can often be designated directly in the grants or in specific budgets allocated for that purpose. Many of the most important funding organisations encourage, and even request, that the projects they fund are made available at no cost to the wider public. IntechOpen strives to maintain excellent relationships with these funders and ensures compliance with mandates.
\n\n
In order to help Authors identify appropriate funding agencies and institutions, we have created a list, based on extensive research on various OA resources (including ROARMAP and SHERPA/JULIET) of organizations that have funds available. Before consulting our list we encourage you to petition your own institution or organization for Open Access funds or check the specifications of your grant with your funder to ascertain if publication costs are included. Where you are in receipt of a grant you should clarify:
\n\n
\n\t
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\n\t
Does your grant list Open Access publication fees as legitimate direct/indirect costs?
\n
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If you are associated with any of the institutions in our list below, you can apply to receive OA publication funds by following the instructions provided in the links. Please consult the Open Access policies or grant Terms and Conditions of any institution with which you are linked to explore ways to cover your publication costs (also accessible by clicking on the link in their title).
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\r\n\tTransforming our World: the 2030 Agenda for Sustainable Development endorsed by United Nations and 193 Member States, came into effect on Jan 1, 2016, to guide decision making and actions to the year 2030 and beyond. Central to this Agenda are 17 Goals, 169 associated targets and over 230 indicators that are reviewed annually. The vision envisaged in the implementation of the SDGs is centered on the five Ps: People, Planet, Prosperity, Peace and Partnership. This call for renewed focused efforts ensure we have a safe and healthy planet for current and future generations.
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\r\n\tThis Series focuses on covering research and applied research involving the five Ps through the following topics:
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\r\n
\r\n\t1. Sustainable Economy and Fair Society that relates to SDG 1 on No Poverty, SDG 2 on Zero Hunger, SDG 8 on Decent Work and Economic Growth, SDG 10 on Reduced Inequalities, SDG 12 on Responsible Consumption and Production, and SDG 17 Partnership for the Goals
\r\n
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\r\n\t2. Health and Wellbeing focusing on SDG 3 on Good Health and Wellbeing and SDG 6 on Clean Water and Sanitation
\r\n
\r\n\t
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\r\n\t3. Inclusivity and Social Equality involving SDG 4 on Quality Education, SDG 5 on Gender Equality, and SDG 16 on Peace, Justice and Strong Institutions
\r\n
\r\n\t
\r\n
\r\n\t4. Climate Change and Environmental Sustainability comprising SDG 13 on Climate Action, SDG 14 on Life Below Water, and SDG 15 on Life on Land
\r\n
\r\n\t
\r\n
\r\n\t5. Urban Planning and Environmental Management embracing SDG 7 on Affordable Clean Energy, SDG 9 on Industry, Innovation and Infrastructure, and SDG 11 on Sustainable Cities and Communities.
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\r\n\tThe series also seeks to support the use of cross cutting SDGs, as many of the goals listed above, targets and indicators are all interconnected to impact our lives and the decisions we make on a daily basis, making them impossible to tie to a single topic.
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\r\n\tIn general, the harsher the environmental conditions in an ecosystem, the lower the biodiversity. Changes in the environment caused by human activity accelerate the impoverishment of biodiversity.
\r\n
\r\n\tBiodiversity refers to “the variability of living organisms from any source, including terrestrial, marine and other aquatic ecosystems and the ecological complexes of which they are part; it includes diversity within each species, between species, and that of ecosystems”.
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\r\n\tBiodiversity provides food security and constitutes a gene pool for biotechnology, especially in the field of agriculture and medicine, and promotes the development of ecotourism.
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\r\n\tCurrently, biologists admit that we are witnessing the first phases of the seventh mass extinction caused by human intervention. It is estimated that the current rate of extinction is between a hundred and a thousand times faster than it was when man first appeared. The disappearance of species is caused not only by an accelerated rate of extinction, but also by a decrease in the rate of emergence of new species as human activities degrade the natural environment. The conservation of biological diversity is "a common concern of humanity" and an integral part of the development process. Its objectives are “the conservation of biological diversity, the sustainable use of its components, and the fair and equitable sharing of the benefits resulting from the use of genetic resources”.
\r\n
\r\n\tThe following are the main causes of biodiversity loss:
\r\n
\r\n\t• The destruction of natural habitats to expand urban and agricultural areas and to obtain timber, minerals and other natural resources.
\r\n
\r\n\t• The introduction of alien species into a habitat, whether intentionally or unintentionally which has an impact on the fauna and flora of the area, and as a result, they are reduced or become extinct.
\r\n
\r\n\t• Pollution from industrial and agricultural products, which devastate the fauna and flora, especially those in fresh water.
\r\n
\r\n\t• Global warming, which is seen as a threat to biological diversity, and will become increasingly important in the future.
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