Pilot Deployment of the LDSD Parachute via a Supersonic Ballute-Reference-Cited by-同舟云学术

Pilot Deployment of the LDSD Parachute via a Supersonic Ballute

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

Tanner Christopher L.¹,O'Farrell Clara¹,Gallon John C.¹,Clark Ian G.¹,Bose Deepak²,Witkowski Allen³,Woodruff Paul J.³

Affiliation:

1. Jet Propulsion Laboratory, California Institute of Technology

2. NASA Ames Research Center

3. Pioneer Aerospace Corporation

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2015-2128

Reference13 articles.

1. Mortar deployment extensibility for the Low Density Supersonic Decelerator parachute

2. LDSD Supersonic Ballute Design and Packing

3. 4Bloetscher, F. “Aerodynamic Deployable Decelerator Performance-Evaluation Program, Phase II,” Tech. Rep. AFFDLTR-67-25, Goodyear Aerospace Corporation, Dayton, OH, June 1967.

4. 5Mayhue, R. and Eckstrom, C. “Flight-Test Results From Supersonic Deployment of an 18-Foot-Diameter (5.49-Meter) Towed Ballute Decelerator,” Tech. Rep. NASA TM X-1773, NASA Langley Research Center, Hampton, VA, May 1969.

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