Assessment of the Reconstructed Aerodynamics of the Mars Science Laboratory Entry Vehicle-Reference-Cited by-同舟云学术

Assessment of the Reconstructed Aerodynamics of the Mars Science Laboratory Entry Vehicle

Published:2014-07 Issue:4 Volume:51 Page:1076-1093
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Schoenenberger Mark¹,Norman John Van¹,Karlgaard Chris¹,Kutty Prasad¹,Way David¹

Affiliation:

1. NASA Langley Research Center, Hampton, Virginia 23681

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.A32794

Reference25 articles.

1. Mars Pathfinder Entry, Descent, and Landing Reconstruction

2. Mars Exploration Rover Six-Degree-of-Freedom Entry Trajectory Analysis

3. Entry, Descent, and Landing Performance of the Mars Phoenix Lander

4. HolmbergN. A.FaustR. P. “Viking ’75 Spacecraft Design and Test Summary, Volume 1—Lander Design,” NASA RP-1027, Nov. 1980.

5. IngoldbyR. N.MichelF. C.FlahertyT. M.DotyM. G.PrestonB.VillyardK. W.SteeleR. D. “Entry Data Analysis for Viking Landers 1 and 2,” Martin Marietta Corp. TN-3770218, Denver, CO, Nov. 1976.

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