Supersonic Retropropulsion Thrust Vectoring for Mars Precision Landing-Reference-Cited by-同舟云学术

Supersonic Retropropulsion Thrust Vectoring for Mars Precision Landing

Published:2015-05 Issue:3 Volume:52 Page:827-835
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Mandalia Amit B.¹,Braun Robert D.¹

Affiliation:

1. Guggenheim School of Aerospace Engineering, Georgia Institute of Technology, Atlanta, Georgia 30332

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.A33119

Reference19 articles.

1. Mars Exploration Entry, Descent, and Landing Challenges

2. High Mass Mars Entry, Descent, and Landing Architecture Assessment

3. Dwyer-CiancioloA. M.DavisJ. L.KomarD. R.MunkM. M.SamarehJ. A.PowellR. W.ShidnerJ. D.StanleyD. O.WilhiteA. W.KinneyD. J.McGuireM. K.ArnoldJ. O.HowardA. R.SostaricR. R.StudakJ. W.ZumwaltC. H.LlamaE. G.CasolivaJ.IvanovM. C.ClarkI.SenguptaA. “Entry, Descent and Landing Systems Analysis Study: Phase 1 Report,” NASA, Tech. Rept. TM-2010-216720, July 2010.

4. DrakeB. G. (ed.), “Human Exploration of Mars: Design Reference Architecture 5.0,” NASA SP-2009-566, 2009.

5. Guidance, Navigation, and Control System Performance Trades for Mars Pinpoint Landing

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