Study of Non-Ablative Lightweight Thermal Protection System for Mars Exploration Mission-Reference-Cited by-同舟云学术

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Study of Non-Ablative Lightweight Thermal Protection System for Mars Exploration Mission

Published:2012-06-25 Issue: Volume: Page:
ISSN:
Container-title:43rd AIAA Thermophysics Conference
language:
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Author:

Suzuki Toshiyuki¹,Aoki Takuya¹,Ogasawara Toshio¹,Ozawa Takashi¹,Fujita Kazuhisa¹,Hatakeyama Yoshikiyo²

Affiliation:

1. Japan Aerospace Exploration Agency (JAXA)

2. Chiba University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2012-3009

Reference7 articles.

1. Nonstop Mars Sample Return System Using Aerocapture Technologies

2. Prediction of Forebody and Aftbody Heat Transfer Rate for Mars Aerocapture Demonstrator

3. Galileo Probe Heat Shield Ablation Experiment

4. Simple Methed of SiC Coating on Carbon/Carbon Composites and Evaluations of Oxidation Resistance

Cited by 3 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Feasibility Improvement of Non-Ablative Lightweight TPS for Mars Aero-flyby Sample Collection Mission;52nd Aerospace Sciences Meeting;2014-01-10

2. Translational temperature distribution measurements in high enthalpy flows by Laser-Induced Fluorescence;51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2013-01-05

3. Experimental Study for Atomic Oxygen Catalytic Efficiency on TPS Surfaces using Microwave Discharged Plasma;51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2013-01-05

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