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A Monte Carlo Analysis of the Thrust Imbalance for the Space Launch System Booster During Both the Ignition Transient and Steady State OperationNo abstract available
Document ID
20140012588
Acquisition Source
Marshall Space Flight Center
Document Type
Presentation
Authors
Foster, Winfred A., Jr. (Auburn Univ. AL, United States)
Crowder, Winston (Lockheed Martin Corp. Huntsville, AL, United States)
Steadman, Todd E. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 25, 2014
Publication Date
July 28, 2014
Subject Category
Launch Vehicles And Launch Operations
Spacecraft Propulsion And Power
Report/Patent Number
M14-3889
Meeting Information
Meeting: AIAA/ASME/SAE/ASEE Joint Propulsion Conference
Location: Cleveland, OH
Country: United States
Start Date: July 28, 2014
End Date: July 30, 2014
Sponsors: Society of Automotive Engineers, Inc., American Society of Mechanical Engineers, American Society for Electrical Engineers, American Inst. of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NNM07AA04A
Distribution Limits
Public
Copyright
Public Use Permitted.

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