Structural Testing of Parachutes in the National Full-Scale Aerodynamics Complex 80- by 120-foot Wind Tunnel at NASA Ames Research Center-Reference-Cited by-同舟云学术

Structural Testing of Parachutes in the National Full-Scale Aerodynamics Complex 80- by 120-foot Wind Tunnel at NASA Ames Research Center

Published:2003-05-19 Issue: Volume: Page:
ISSN:
Container-title:17th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar
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Author:

Zell Pete¹,Cruz Juan²,Witkowski Allan³

Affiliation:

1. NASA Ames Research Center

2. NASA Langley Research Center

3. Pioneer Aerospace Corporation

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2003-2130

Reference9 articles.

1. Aerodynamic decelerator testing in the National Full-Scale Aerodynamics Complex

2. McBride, D.B. "Orbiter Drag Chute Stability Test in the NASA/Ames 80-by-120-Foot Wind Tunnel," Sandia Report SAND 93-2544, Sandia National Laboratories,February1994.

3. "Test Planning Guide for Investigations in the 40- by 80- and 80-by-120-Foot Wind Tunnel Facility," NASA Ames Wind Tunnel Operations Division document,revisedsummer1993.

4. Zell, P.T. "Performance and Test Section Flow Characteristics of the National Full-Scale Aerodynamics Complex 80-by-120-Foot Wind Tunnel," NASA Technical Memorandum 103920, January1993.

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