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Space shuttle solid rocket booster main parachute damage reduction team reportThis report gives the findings of the space shuttle solid rocket booster main parachute damage reduction team. The purpose of the team was to investigate the causes of main parachute deployment damage and to recommend methods to eliminate or substantially reduce the damage. The team concluded that the two primary causes of significant damage during deployment are vent entanglement and contact of the parachutes with the main parachute support structure. As an inexpensive but effective step towards damage reduction, the team recommends modification of the parachute packing procedure to eliminate vent entanglement. As the most effective design change, the team recommends a pilot chute-deployed soft-pack system. Alternative concepts are also recommended that provide a major reduction in damage at a total cost lower than the pilot chute-deployed soft pack.
Document ID
19930008878
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Watts, G.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1993
Subject Category
Launch Vehicles And Space Vehicles
Report/Patent Number
M-706
NASA-TM-4437
NAS 1.15:4437
Accession Number
93N18067
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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