Radiative Transfer in a Low-Density Ablative Material Under Arcjet Flow Conditions
Author:
Affiliation:
1. Tottori University, Tottori 680-8552, Japan
2. Japan Aerospace Exploration Agency, Chofu-shi 181-0012, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Condensed Matter Physics,Aerospace Engineering,Space and Planetary Science,Fluid Flow and Transfer Processes,Mechanical Engineering
Reference24 articles.
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2. TranH.JohnsonC.RaskyD.HuiF.ChenY. K.HsuM. “Phenolic Impregnated Carbon Ablators (PICA) for Discovery Missions,” NASA TM 110440, April 1997.
3. Performance of a Low Density Ablative Heat Shield Material
4. Sizing and Margins Assessment of the Mars Science Laboratory Aeroshell Thermal Protection System
5. Ablation Sensor Unit for Flight Demonstration on HTV Small Recovery Capsule
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