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First Test Flight Thermal Performance of the Low Density Supersonic Decelerator (LDSD) Supersonic Flight Dynamics Test (SFDT) VehicleThe thermal telemetry from the first test flight, an assessment of post-flight inspections of the recovered vehicle, and a review of the thermal design and model of the vehicle will be presented along with several lessons learned.
Document ID
20170007025
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
External Source(s)
hdl:2014/45732
Authors
Mastropietro, A.J. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Kempenaar, Jason (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Redmond, Matthew (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Pauken, Michael (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Ancarrow, Walt (WCA Engineering, Inc Jarrettsville, MD)
Date Acquired
August 1, 2017
Publication Date
July 12, 2015
Subject Category
Aerodynamics
Aircraft Design, Testing And Performance
Meeting Information
Meeting: International Conference on Environmental Systems 2015
Location: Bellevue, WA
Country: United States
Start Date: July 12, 2015
End Date: July 16, 2015
Sponsors: Texas Tech Univ.
Distribution Limits
Public
Copyright
Other
Keywords
flight test data
telemetry
thermal analysis
decelerator

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