Postflight Thermal Protection System Analysis of Hayabusa Reentry Capsule-Reference-Cited by-同舟云学术

Postflight Thermal Protection System Analysis of Hayabusa Reentry Capsule

Published:2014-01 Issue:1 Volume:51 Page:96-105
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Suzuki Toshiyuki,Fujita Kazuhisa,Yamada Tetsuya,Inatani Yoshifumi,Ishii Nobuaki

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.A32549

Reference34 articles.

1. Reentry of Hayabusa Sample Return Capsule and Post-Flight Analysis of the Recovered Heatshield

2. Numerical Reconstruction of HAYABUSA Sample Return Capsule Flight Environments

3. MoyerC. B.RindalR. A. “An Analysis of the Coupled Chemically Reacting Boundary Layer and Charring Ablator, Part II: Finite Different Solution for the In-Depth Response of Charring Materials Considering Surface Chemical and Energy Balances,” NASA CR-1061, June 1968.

4. Ablation and Thermal Response Program for Spacecraft Heatshield Analysis

5. Response of Heatshield Material at Stagnation Point of Pioneer-Venus Probes

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