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Reverse Launch Abort System Parachute Architecture Trade StudyThis study investigated a potential Launch Abort System (LAS) Concept of Operations and abort parachute architecture. The purpose of the study was to look at the concept of jettisoning the LAS tower forward (Reverse LAS or RLAS) into the free-stream flow rather than after reorienting to a heatshield forward orientation. A hypothesized benefit was that due to the compressed timeline the dynamic pressure at main line stretch would be substantially less. This would enable the entry parachutes to be designed and sized based on entry loading conditions rather than the current stressing case of a Pad Abort. Ultimately, concerns about the highly dynamic reorientation of the CM via parachutes, and the additional requirement of a triple bridle attachment for the RLAS parachute system, overshadowed the potential benefits and ended this effort.
Document ID
20110004069
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Litton, Daniel K.
(NASA Langley Research Center Hampton, VA, United States)
O'Keefe, Stephen A.
(Analytical Mechanics Associates, Inc. Hampton, VA, United States)
Winski, Richard G.
(Binera, Inc. VA, United States)
Date Acquired
August 25, 2013
Publication Date
January 4, 2011
Subject Category
Launch Vehicles And Launch Operations
Report/Patent Number
AIAA Paper 2011-1225
NF1676L-11872
Report Number: AIAA Paper 2011-1225
Report Number: NF1676L-11872
Meeting Information
Meeting: 49th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition
Location: Orlando, FL
Country: United States
Start Date: January 4, 2011
End Date: January 7, 2011
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Public Use Permitted.
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