NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
SRB water impact velocity trade studyThe results of the attrition/cost studies which formulated the data base for the recommendation to reduce the Space Shuttle Solid Rocket Booster's nominal vertical water impact velocity to 85 feet per second is presented.
Document ID
19760015072
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Counter, D. N. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Crockett, C. D. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 3, 2013
Publication Date
April 1, 1976
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-X-64997
Report Number: NASA-TM-X-64997
Accession Number
76N22160
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

There are no records associated with this record.
No Preview Available