Guided Entry Performance of Low Ballistic Coefficient Vehicles at Mars-Reference-Cited by-同舟云学术

Guided Entry Performance of Low Ballistic Coefficient Vehicles at Mars

Published:2013-09 Issue:5 Volume:50 Page:1047-1059
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Meginnis Ian M.¹,Putnam Zachary R.¹,Clark Ian G.¹,Braun Robert D.¹,Barton Gregg H.²

Affiliation:

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

2. Mission Design and Analysis, Charles Stark Draper Laboratory, Houston, Texas 77058

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.A32425

Reference16 articles.

1. Mars Exploration Entry, Descent, and Landing Challenges

2. An Evaluation of Ballute Entry Systems for Lunar Return Missions

3. Survey of Ballute Technology for Aerocapture

4. Dwyer CiancioloA.EngelundW. C.PowellR. W.ManningR. M.CerimeleC. J.WesthelleC. H.ArnoldJ. O.KinneyD. J. “Entry, Descent and Landing Systems Analysis Study: Phase 1 Report,” NASA TM-2010-216720, July 2010.

5. AdlerM.WrightM.CampbellC.ClarkI.EngelundW.RivelliniT. “Draft Entry, Descent, and Landing Roadmap: Technology Area 09,” NASA, Nov. 2010.

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