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SFDT-1 Camera Pointing and Sun-Exposure Analysis and Flight PerformanceThe Supersonic Flight Dynamics Test (SFDT) vehicle was developed to advance and test technologies of NASA's Low Density Supersonic Decelerator (LDSD) Technology Demonstration Mission. The first flight test (SFDT-1) occurred on June 28, 2014. In order to optimize the usefulness of the camera data, analysis was performed to optimize parachute visibility in the camera field of view during deployment and inflation and to determine the probability of sun-exposure issues with the cameras given the vehicle heading and launch time. This paper documents the analysis, results and comparison with flight video of SFDT-1.
Document ID
20150006857
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
White, Joseph
(Analytical Mechanics Associates, Inc. Hampton, VA, United States)
Dutta, Soumyo
(NASA Langley Research Center Hampton, VA, United States)
Striepe, Scott
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
April 28, 2015
Publication Date
January 11, 2015
Subject Category
Spacecraft Design, Testing And Performance
Aircraft Stability And Control
Report/Patent Number
NF1676L-19669
AAS 15-218
Meeting Information
Meeting: AAS/AIAA Space Flight Mechanics Meeting
Location: Williamsburg, VA
Country: United States
Start Date: January 11, 2015
End Date: January 15, 2015
Sponsors: American Astronautical Society, American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 406979.01.07.06
Distribution Limits
Public
Copyright
Public Use Permitted.
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