Design, Development and Flight-Testing of the U.S. Army 4200 ft2 Parafoil Recovery System-Reference-Cited by-同舟云学术

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Design, Development and Flight-Testing of the U.S. Army 4200 ft2 Parafoil Recovery System

Published:2005-05-23 Issue: Volume: Page:
ISSN:
Container-title:18th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar
language:
Short-container-title:

Author:

Bennett Thomas¹,Fox Roy²

Affiliation:

1. Pioneer Aerospace

2. Fox Parachute Services

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2005-1628

Reference4 articles.

1. An Overview of the Guided Parafoil System Derived from X-38 Experience

2. 4Madsen,C.,NASAJSCpresentation,"LCWW-3TestConfigurationReview",dated10/3/03

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. An Overview of the Guided Parafoil System Derived from X-38 Experience;18th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar;2005-05-23

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