Aerothermal heating predictions for Mars Microprobe

Author:

Mitcheltree R.1,DiFulvio M.1,Horvath T.1,Braun R.1

Affiliation:

1. NASA, Langley Research Center, Hampton, VA

Publisher

American Institute of Aeronautics and Astronautics

Cited by 9 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. Numerical investigation of a hypersonic flow around a capsule in CO2–N2 environment;European Journal of Mechanics - B/Fluids;2020-03

2. Evidence-Based Multi-disciplinary Robust Optimization for Mars Microentry Probe Design;EVOLVE – A Bridge between Probability, Set Oriented Numerics and Evolutionary Computation VII;2017

3. Evidence Theory Based Multidisciplinary Robust Optimization for Micro Mars Entry Probe Design;EVOLVE - A Bridge between Probability, Set Oriented Numerics, and Evolutionary Computation IV;2013

4. A Review of Aerothermal Modeling for Mars Entry Missions;48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition;2010-01-04

5. Multi-Objective Hypersonic Entry Aeroshell Shape Optimization;Journal of Spacecraft and Rockets;2009-09

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