A Cellular Backshell Concept for a Planetary Entry Vehicle-Reference-Cited by-同舟云学术

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A Cellular Backshell Concept for a Planetary Entry Vehicle

Published:2018-09-15 Issue: Volume: Page:
ISSN:
Container-title:2018 AIAA SPACE and Astronautics Forum and Exposition
language:
Short-container-title:

Author:

Krings Ethan¹,Stubing Richard¹,Walker Sandra P.¹,Langston Sarah¹

Affiliation:

1. NASA Langley Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2018-5194

Reference14 articles.

1. Aerothermodynamic Design of the Mars Science Laboratory Heatshield

2. Anon.,http://www.spacex.com/sites/spacex/files/pdf/DragonLabFactSheet.pdf[cited18November2013]

3. Bose,D.M.,etal."TheHypersonicInflatableAerodynamicDecelerator(HIAD)MissionApplicationsStudy," AIAA AerodynamicDeceleratorSystems TechnologyConferenceandSeminar,Daytona Beach,FL,2013.

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