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Hyper-X Stage Separation: Simulation Development and ResultsThis paper provides an overview of stage separation simulation development and results for NASA's Hyper-X program; a focused hypersonic technology effort designed to move hypersonic, airbreathing vehicle technology from the laboratory environment to the flight environment. This paper presents an account of the development of the current 14 degree of freedom stage separation simulation tool (SepSim) and results from use of the tool in a Monte Carlo analysis to evaluate the risk of failure for the separation event. Results from use of the tool show that there is only a very small risk of failure in the separation event.
Document ID
20010058883
Acquisition Source
Langley Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Reubush, David E.
(NASA Langley Research Center Hampton, VA United States)
Martin, John G.
(NASA Langley Research Center Hampton, VA United States)
Robinson, Jeffrey S.
(NASA Langley Research Center Hampton, VA United States)
Bose, David M.
(Analytical Mechanics Associates, Inc. Hampton, VA United States)
Strovers, Brian K.
(Analytical Mechanics Associates, Inc. Hampton, VA United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2001
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
AIAA Paper 2001-1802
Report Number: AIAA Paper 2001-1802
Meeting Information
Meeting: 10th AIAA/NAL-NASDA-ISAS International Space Planes and Hypersonic Systems and Technologies Conference Committee
Location: Kyoto
Country: Japan
Start Date: April 24, 2001
End Date: April 27, 2001
Sponsors: National Space Development Agency, American Inst. of Aeronautics and Astronautics, National Aeronautical Lab., Tokyo Univ.
Distribution Limits
Public
Copyright
Public Use Permitted.
No Preview Available