Design of Subscale Parachute Models for LDSD Transonic Dynamics Wind Tunnel Testing-Reference-Cited by-同舟云学术

Design of Subscale Parachute Models for LDSD Transonic Dynamics Wind Tunnel Testing

Published:2015-03-27 Issue: Volume: Page:
ISSN:
Container-title:23rd AIAA Aerodynamic Decelerator Systems Technology Conference
language:
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Author:

Witkowski Allen¹,Machalick Walter¹,O'Farrell Clara²

Affiliation:

1. Pioneer Aerospace Corporation

2. Jet Propulsion Laboratory, California Institute of Technology

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2015-2110

Reference6 articles.

1. Wind Tunnel Testing of Various Disk-Gap-Band Parachutes

2. J. Cruz, C. O'Farrell, and Clark, I.G "Statement Of Work, Parachute Models For The 2014 Wind Tunnel Test At TheNASA Langley TransonicDynamicsTunnel(TDT),"Version14,September 22,2014.

3. J. Reuter, W. Machalick, A. Witkowski, M. Kandis, A. Sengupta, R. Kelsch, "Design of Subscale Parachute Modelsfor MSLSupersonicWind Tunnel",2009-2999.May2009.

4. DesignReportfortheMERWindTunnelModels,PACDoc.EA2036-7B,April6,2001,RevisedMay8,2001.

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