Thermal performance of advanced charring ablator systems for future robotic and manned missions to Mars-Reference-Cited by-同舟云学术

Thermal performance of advanced charring ablator systems for future robotic and manned missions to Mars

Published:2001-06-11 Issue: Volume: Page:
ISSN:
Container-title:35th AIAA Thermophysics Conference
language:
Short-container-title:

Author:

Congdon William¹,Curry Donald²

Affiliation:

1. Applied Research Associates, Inc., Englewood, CO

2. NASA, Johnson Space Center, Houston, TX

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2001-2829

Reference14 articles.

1. D.A.Rarick, "Arc-Jet Testing of Advanced Ablative Materials Manufactured by Applied Research Associates, Inc."NASA Johnson Space Center, Technical Report JSC-28984, May 2000.

2. W.M.Congdon, 'Test and Analysis of the Thermal Protection System for the Mars Pathfinder Entry Vehicle," ARA Contract Report ARA-5938-R-062, NASA/JPL Contract 959983,May 1995.

Cited by 4 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. Arcjet Screening of Candidate Ablative Thermal Protection Materials for Mars Science Laboratory;Journal of Spacecraft and Rockets;2006-03

2. Response Modeling of Lightweight Charring Ablators and Thermal Radiation Testing Results;39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit;2003-06-26

3. Arc Jet Screening of Candidate Ablative Thermal Protection Materials for Mars Smart Lander;AIAA Atmospheric Flight Mechanics Conference and Exhibit;2002-06-25

4. Validation Arc-Jet Testing and Thermal-Response Modeling of Advanced Lightweight Charring-Ablator Families;8th AIAA/ASME Joint Thermophysics and Heat Transfer Conference;2002-06-24