Opportunities and Limitations in Low-Earth Subsonic Testing and Qualification of Extraterrestrial Supersonic Parachute Designs-Reference-Cited by-同舟云学术

Opportunities and Limitations in Low-Earth Subsonic Testing and Qualification of Extraterrestrial Supersonic Parachute Designs

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

Steltzner Adam¹,Bruno Robin¹,Mitcheltree Robert¹,Cruz Juan²

Affiliation:

1. Jet Propulsion Laboratory

2. NASA Langley Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2003-2135

Reference22 articles.

1. An Entry, Descent and Landing System for the Beagle2 Mars mission

2. ) Jaremenko, I., Steinberg, S., and Faye-Petersen, R.: Scale model test results of the Viking parachute system at Mach number from 0.1 through 2.6, NASACR-149377,1971.

3. ) Murrow, H.N., Eckstrom, C.V., and Henke, D.W.; Development flight tests of the Viking decelerator system, AIAA Paper73-455,1973.

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