A novel ablative material for thermal protection system: Carbon fiber/polysiloxane composites-Reference-Cited by-同舟云学术

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A novel ablative material for thermal protection system: Carbon fiber/polysiloxane composites

Published:2022-10 Issue: Volume:129 Page:107822
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Hou Yanan^ORCID,Yee Colin^ORCID,Li Wei^ORCID,Koo Joseph H.,Li Liguo,Rech Ben,Fahy William^ORCID,Wu Hao,Buffy Jarrod J.

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference17 articles.

1. Apollo experience report: thermal protection subsystem;Pavlosky;Apollo Int. Mag. Art Antiq.,1974

2. Apollo thermal-protection system development;Bryan Erb;J. Spacecr. Rockets,1970

3. Studies of Ablative Material Performance for Solid Rocket Nozzle Applications;Schaefer,1967

4. Venkatapathy - 2003 - thermal protection system technology and facility needs for demanding future planetery missions;Laub,2004

5. An evaluation of ablation mechanisms for the apollo heat shield material;Bartlett;J. Spacecr. Rockets,1971

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