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Low Density Supersonic Decelerators (LDSD): Reconstructed Parachute System Performance During the Second Supersonic Flight Dynamics TestNo abstract available
Document ID
20190033641
Acquisition Source
Jet Propulsion Laboratory
Document Type
Presentation
External Source(s)
hdl:2014/46735
Authors
O'Farrell, Clara (Jet Propulsion Laboratory (JPL), California Institute of Technology (CalTech) Pasadena, CA, United States)
Brandeau, Erich (Jet Propulsion Laboratory (JPL), California Institute of Technology (CalTech) Pasadena, CA, United States)
Tanner, Chris (Jet Propulsion Laboratory (JPL), California Institute of Technology (CalTech) Pasadena, CA, United States)
Gallon, John (Jet Propulsion Laboratory (JPL), California Institute of Technology (CalTech) Pasadena, CA, United States)
Clark, Ian (Jet Propulsion Laboratory (JPL), California Institute of Technology (CalTech) Pasadena, CA, United States)
Muppidi, Suman (Analytical Mechanics Associates, Inc. Moffett Field, CA, United States)
Date Acquired
December 12, 2019
Publication Date
June 13, 2016
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
JPL-CL-16-2320
Report Number: JPL-CL-16-2320
Meeting Information
Meeting: AIAA Atmospheric Flight Mechanics Conference
Location: Washington, D. C.
Country: United States
Start Date: June 13, 2016
End Date: June 17, 2016
Sponsors: American Institute of Aeronautics and Astronautics (AIAA)
Distribution Limits
Public
Copyright
Other

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