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Quantification of the Uncertainties for the Space Launch System Liftoff/Transition and Ascent DatabasesA detailed description of the uncertainty quantification process for the Space Launch System Block 1 vehicle configuration liftoff/transition and ascent 6-Degree-of-Freedom (DOF) aerodynamic databases is presented. These databases were constructed from wind tunnel test data acquired in the NASA Langley Research Center 14- by 22-Foot Subsonic Wind Tunnel and the Boeing Polysonic Wind Tunnel in St. Louis, MO, respectively. The major sources of error for these databases were experimental error and database modeling errors.
Document ID
20160007692
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Favaregh, Amber L. (Vigyan Research Associates, Inc. Hampton, VA, United States)
Houlden, Heather P. (Vigyan Research Associates, Inc. Hampton, VA, United States)
Pinier, Jeremy T. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
June 20, 2016
Publication Date
January 4, 2016
Subject Category
Aerodynamics
Launch Vehicles And Launch Operations
Ground Support Systems And Facilities (Space)
Report/Patent Number
NF1676L-22968
Meeting Information
Meeting: AIAA SciTech Forum 2016
Location: San Diego, CA
Country: United States
Start Date: January 4, 2016
End Date: January 8, 2016
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 585777.02.40.04.03.50.04
CONTRACT_GRANT: NNL12AA09C
Distribution Limits
Public
Copyright
Public Use Permitted.

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