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STS-3 main parachute failureA failure analysis of the parachute on the Space Transportation System 3 flight's solid rocket booster's is presented. During the reentry phase of the two Solid Rocket Boosters (SRBs), one 115 ft diameter main parachute failed on the right hand SRB (A12). This parachute failure caused the SRB to impact the Ocean at 110 ft/sec in lieu of the expected 3 parachute impact velocity of 88 ft/sec. This higher impact velocity relates directly to more SRB aft skirt and more motor case damage. The cause of the parachute failure, the potential risks of losing an SRB as a result of this failure, and recommendations to ensure that the probability of chute failures of this type in the future will be low are discussed.
Document ID
19820021473
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Runkle, R.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Henson, K.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 4, 2013
Publication Date
June 1, 1982
Subject Category
Space Transportation
Report/Patent Number
NASA-TM-82490
NAS 1.15:82490
Report Number: NASA-TM-82490
Report Number: NAS 1.15:82490
Accession Number
82N29349
Funding Number(s)
PROJECT: RTOP 984-11-16
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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