Survey of Supersonic Retropropulsion Technology for Mars Entry, Descent, and Landing-Reference-Cited by-同舟云学术

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Survey of Supersonic Retropropulsion Technology for Mars Entry, Descent, and Landing

Published:2009-09 Issue:5 Volume:46 Page:929-937
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Korzun Ashley M.¹,Braun Robert D.¹,Cruz Juan R.²

Affiliation:

1. Georgia Institute of Technology, Atlanta, Georgia 30332-0150

2. NASA Langley Research Center, Hampton, Virginia 23681-2199

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.41161

Reference53 articles.

1. Static aerodynamics 1.05-6.0, 20-21 Air Air, helium [10,11,13-26,31,41-44]

2. Flowfield stability 1.05-6.0 Air Air, helium [10,11,13,16-18,23]

3. Flowfield geometry 1.05-8.0 Air Air, helium [10,11,13-17,19-21,25,41-44]

4. Effect of nozzle geometry 1.05-6.0, 20-21 Air Air, helium [10,11,13-15,24,26,42]

5. Angle of attack variation 1.05-6.0 Air Air, helium [10,11,14,16,17]

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2. Re-entry rocket basic flow characteristics and thermal environment of different retro-propulsion modes;Chinese Journal of Aeronautics;2024-07

3. Numerical Investigation of Gas Models for Retropropulsion Flows for Future Mars Missions;Journal of Spacecraft and Rockets;2024-06-25

4. Sustainable space technologies—Strategies toward a predictive aerothermal design of re-useable space transportation systems;Review of Scientific Instruments;2024-02-01

5. Unsteady Aerodynamics of the Retropropulsion Reentry Burn of Vertically Landing Launchers;Journal of Spacecraft and Rockets;2023-11

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