Multidimensional Effects on Heatshield Thermal Response for the Orion Crew Module-Reference-Cited by-同舟云学术

Multidimensional Effects on Heatshield Thermal Response for the Orion Crew Module

Published:2007-06-15 Issue: Volume: Page:
ISSN:
Container-title:39th AIAA Thermophysics Conference
language:
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Author:

Chen Yih-Kanq¹,Milos Frank¹

Affiliation:

1. NASA Ames Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2007-4397

Reference16 articles.

1. Chen, Y.K., and Milos, F.S. "Three-Dimensional Ablation and Thermal Response Simulation System," AIAA Paper 2005-5064,June2005.

2. Ablation and Thermal Response Program for Spacecraft Heatshield Analysis

3. Moyer, C.B., and Rindal, R.A. "An Analysis of the Coupled Chemically Reacting Boundary Layer and Charring Ablator, Part II, Finite Difference Solution for the In-Depth Response of Charring Materials Considering Surface Chemical and Energy Balances," NASA CR-1061,1968.

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