Mars Phoenix Scout Parachute Canopy Structural Test Peak Load Prediction Technique-Reference-Cited by-同舟云学术

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Mars Phoenix Scout Parachute Canopy Structural Test Peak Load Prediction Technique

Published:2007-05-21 Issue: Volume: Page:
ISSN:
Container-title:19th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar
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Author:

Taeger Yaro¹,Witkowski Allen¹,Kandis Mike¹

Affiliation:

1. Pioneer Aerospace Corporation

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2007-2566

Reference4 articles.

1. Opening Loads Analyses for Various Disk-Gap-Band Parachutes

Cited by 1 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. Stress Analysis of the Parachute System for the Mars Science Laboratory Mission;20th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar;2009-05-04

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