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Test report for 120-inch-diameter Solid Rocket Booster (SRB) model testsThe space shuttle solid rocket boosters (SRB's) will be jettisoned to impact in the ocean within a 200-mile radius of the launch site. Tests were conducted at Long Beach, California, using a 12-inch diameter Titan 3C model to simulate the full-scale characteristics of the prototype SRB during retrieval operations. The objectives of the towing tests were to investigate and assess the following: (1) a floating and towing characteristics of the SRB; (2) need for plugging the SRB nozzle prior to tow; (3) attach point locations on the SRB; (4) effects of varying the SRB configuration; (5) towing hardware; and (6) difficulty of attaching a tow line to the SRB in the open sea. The model was towed in various sea states using four different types and varying lengths of tow line at various speeds. Three attach point locations were tested. Test data was recorded on magnetic tape for the tow line loads and for model pitch, roll, and yaw characteristics and was reduced by computer to tabular printouts and X-Y plots. Profile and movie photography provided documentary test data.
Document ID
19740003486
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Jones, W. C.
(NASA John F. Kennedy Space Center Cocoa Beach, FL, United States)
Date Acquired
September 3, 2013
Publication Date
August 1, 1973
Subject Category
Propulsion Systems
Report/Patent Number
NASA-TM-X-69441
KSC-TR-1253
Report Number: NASA-TM-X-69441
Report Number: KSC-TR-1253
Accession Number
74N11599
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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