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Low Density Supersonic Decelerator (LDSD) Supersonic Flight Dynamics Test (SFDT) Plume Induced Environment ModellingProvide plume induced heating (radiation & convection) predictions in support of the LDSD thermal design (pre-flight SFDT-1) Predict plume induced aerodynamics in support of flight dynamics, to achieve targeted freestream conditions to test supersonic deceleration technologies (post-flight SFDT-1, pre-flight SFDT-2)
Document ID
20160008864
Acquisition Source
Marshall Space Flight Center
Document Type
Presentation
Authors
Mobley, B. L. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Smith, S. D. (Plumetech, Inc. Huntsville, AL, United States)
Van Norman, J. W. (Analytical Mechanics Associates, Inc. Hampton, VA, United States)
Muppidi, S. (ERC, Inc. Moffett Field, CA, United States)
Clark, I (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
July 8, 2016
Publication Date
June 13, 2016
Subject Category
Aerodynamics
Spacecraft Design, Testing And Performance
Report/Patent Number
M16-5363
Meeting Information
Meeting: International Planetary Probe Conference
Location: Laurel, MD
Country: United States
Start Date: June 13, 2016
End Date: June 17, 2016
Sponsors: Johns Hopkins Univ.
Distribution Limits
Public
Copyright
Public Use Permitted.

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