Sizing and Margins Assessment of Mars Science Laboratory Aeroshell Thermal Protection System-Reference-Cited by-同舟云学术

Sizing and Margins Assessment of Mars Science Laboratory Aeroshell Thermal Protection System

Published:2014-07 Issue:4 Volume:51 Page:1125-1138
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Wright Michael J.¹,Beck Robin A. S.¹,Edquist Karl T.²,Driver David¹,Sepka Steven A.³,Slimko Eric M.⁴,Willcockson William H.⁵

Affiliation:

1. NASA Ames Research Center, Moffett Field, California 94035

2. NASA Langley Research Center, Hampton, Virginia 23681

3. ERC, Inc., Sunnyvale, California 94087

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

5. Lockheed Martin Space Systems, Littleton, Colorado 80125

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.A32579

Reference21 articles.

1. Mars Science Laboratory Entry, Descent, and Landing System

2. BeckR. A. S.DriverD. M.WrightM. J.LaubB.SlimkoE. M.EdquistK. T.ThamesT.WillcocksonW. H.SepkaS.HwangH. H. “Development of the MSL Heatshield TPS,” AIAA Paper 2009-4229, June 2009.

3. Aerothermodynamic Design of the Mars Science Laboratory Heatshield

4. Aerothermodynamic Design of the Mars Science Laboratory Backshell and Parachute Cone

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

Cited by 39 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Pyrolysis front detection in carbon phenolic composites using x-ray computed tomography;Composites Part A: Applied Science and Manufacturing;2024-12

2. Flow Mechanics in Ablative Thermal Protection Systems;Annual Review of Fluid Mechanics;2024-01-19

3. Effect of the Internal Gas Flow Velocity on the Thermal Conductivity of Porous Thermal Protection Systems and Application to Stardust Re-Entry;AIAA SCITECH 2024 Forum;2024-01-04

4. Experimental investigation on the validity of the local thermal equilibrium assumption in ablative-material response models;Aerospace Science and Technology;2023-10

5. Mixed Oxide Aerogels with High‐Performance Insulating Properties for High‐Temperature Space Application;Advanced Engineering Materials;2023-08-23