An Asymmetric Capsule Vehicle Geometry Study for CEV

Author:

Brown James1,Garcia Joseph1,Kinney David1,Prabhu Dinesh2

Affiliation:

1. NASA Ames Research Center

2. ELORET Corporation

Publisher

American Institute of Aeronautics and Astronautics

Reference40 articles.

1. 1"NASA'sExplorationSystemsArchitectureStudy,"NASATM-2005-325062,November2005.

2. 2"TheApolloSpacecraft-AChronology,"NASASP-4009,1969.

3. 5Abbot,I.H.andDoenhoff,A.E.,TheoryofWingSections,Dover,1959.

Cited by 3 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. Parametric Cost Estimates of Four 20 Ton Payload Mars EDL Vehicle Concepts;AIAA Scitech 2020 Forum;2020-01-05

2. Computational-Fluid-Dynamics-Based Axisymmetric Aeroshell Shape Optimization in Hypersonic Entry Conditions;Journal of Spacecraft and Rockets;2015-01

3. On Heatshield Shapes for Mars Entry Capsules;50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2012-01-09

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