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Aerodynamic Disturbance Force and Torque Estimation for Spacecraft and Simple Shapes Using Finite Plate Elements – Part I: Drag Coefficient

By Charles Reynerson

Submitted: April 27th 2010Published: February 14th 2011

DOI: 10.5772/13331

Downloaded: 3087

© 2011 The Author(s). Licensee IntechOpen. This chapter is distributed under the terms of the Creative Commons Attribution-NonCommercial-ShareAlike-3.0 License, which permits use, distribution and reproduction for non-commercial purposes, provided the original is properly cited and derivative works building on this content are distributed under the same license.

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Charles Reynerson (February 14th 2011). Aerodynamic Disturbance Force and Torque Estimation for Spacecraft and Simple Shapes Using Finite Plate Elements – Part I: Drag Coefficient, Advances in Spacecraft Technologies Jason Hall, IntechOpen, DOI: 10.5772/13331. Available from:

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