Development of Supersonic Retropropulsion for Future Mars Entry, Descent, and Landing Systems-Reference-Cited by-同舟云学术

Development of Supersonic Retropropulsion for Future Mars Entry, Descent, and Landing Systems

Published:2014-05 Issue:3 Volume:51 Page:650-663
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Edquist Karl T.¹,Korzun Ashley M.¹,Dyakonov Artem A.²,Studak Joseph W.³,Kipp Devin M.⁴,Dupzyk Ian C.⁵

Affiliation:

1. Atmospheric Flight & Entry Systems Branch, NASA Langley Research Center, Hampton, Virginia 23681

2. Blue Origin, LLC, Kent, Washington 98032

3. Propulsion Systems Branch, NASA Johnson Space Center, Houston, Texas 77058

4. Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California, 91109

5. Lunexa, LLC, San Francisco, California 94105

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.A32715

Reference30 articles.

1. Mars Exploration Entry, Descent, and Landing Challenges

2. Dwyer-CiancoloA.DavisJ.KomarD.MunkM.SamarehJ.Williams-ByrdJ.ZangT.PowellR.ShidnerJ.StanleyD.WilhiteA.KinneyD.McGuireK.ArnoldJ.HowardA.SostaricR.StudakJ.ZumwaltC.LlamaE.CasolivaJ.IvanovM.ClarkI.SenguptaA. “Entry, Descent and Landing Systems Analysis Study: Phase 1 Report,” NASA TM-2010-216720, July 2010.

3. AdlerM.WrightM.CampbellC.ClarkI.EngelundW.RivelliniT. “Entry, Descent, and Landing Roadmap: Technology Area 09,” NASA, April 2012.

4. Conceptual Modeling of Supersonic Retropropulsion Flow Interactions and Relationships to System Performance

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