Development of the Mars Science Laboratory Heatshield Thermal Protection System-Reference-Cited by-同舟云学术

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Development of the Mars Science Laboratory Heatshield Thermal Protection System

Published:2014-07 Issue:4 Volume:51 Page:1139-1150
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Beck Robin A. S.¹,Driver David M.¹,Wright Michael J.¹,Hwang Helen H.¹,Edquist Karl T.²,Sepka Steven A.³

Affiliation:

1. Entry Systems and Vehicle Development Branch, NASA Ames Research Center, Moffett Field, California 94035

2. Atmospheric Flight and Entry Systems Branch, NASA Langley Research Center, Hampton, Virginia 23681

3. ERC, Inc., Moffett Field, California 94035

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.A32635

Reference14 articles.

1. Aerothermodynamic Design of the Mars Science Laboratory Heatshield

2. Development of a High-Fidelity Thermal/Ablation Response Model for SLA-561V

3. A Theory for the Ablation of Glassy Materials

4. Arc Jet Testing in a Shear Environment for Mars Science Laboratory Thermal Protection System

5. Post-Flight Analysis of the Stardust Sample Return Capsule Earth Entry

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