Engineering

Vol.4 No.6(2012), Paper ID 19848, 14 pages

DOI:10.4236/eng.2012.46040

 

Effect of Spacecraft Aerodynamics and Heat Shield Characteristics on Optimal Aeroassisted Transfer

 

Antonio Mazzaracchio, Mario Marchetti

 

Astronautical, Electrical, and Energetic Engineering Department, Sapienza University of Rome, Rome, Italy
Astronautical, Electrical, and Energetic Engineering Department, Sapienza University of Rome, Rome, Italy

 

Copyright © 2012 Antonio Mazzaracchio, Mario Marchetti et al. This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.

 

How to Cite this Article


A. Mazzaracchio and M. Marchetti, "Effect of Spacecraft Aerodynamics and Heat Shield Characteristics on Optimal Aeroassisted Transfer," Engineering, Vol. 4 No. 6, 2012, pp. 307-320. doi: 10.4236/eng.2012.46040.

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