Aerothermodynamic design feasibility of a generic planetary aerocapture/aeromaneuver vehicle
Author:
Affiliation:
1. General Electric Co., Re-Entry Systems Div., Philadelphia, PA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1981-1127
Reference52 articles.
Cited by 11 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献
1. Measured and predicted heating distributions for biconics at Mach 10;Journal of Spacecraft and Rockets;1986-05
2. Measured and Predicted Vortex-Induced Leeward Heating on a Biconic at Mach 6 and 10;Thermophysical Aspects of Re-Entry Flows;1986-01-01
3. Thermal design of AOTV heatshields for a conical drag brake;20th Thermophysics Conference;1985-06-19
4. Aerodynamics of generalized bent biconics for aero-assisted, orbital-transfer vehicles;Journal of Spacecraft and Rockets;1985-03
5. Trajectory analysis of radiative heating for planetary missions withaerobraking of spacecraft;Journal of Spacecraft and Rockets;1985-01
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