NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Liquid Booster Module (LBM) plume flowfield modelA complete definition of the LBM plume is important for many Shuttle design criteria. The exhaust plume shape has a significant effect on the vehicle base pressure. The LBM definition is also important to the Shuttle base heating, aerodynamics and the influence of the exhaust plume on the launch stand and environment. For these reasons a knowledge of the LBM plume characteristics is necessary. A definition of the sea level LBM plume as well as at several points along the Shuttle trajectory to LBM, burnout is presented.
Document ID
19810009563
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Smith, S. D.
(Lockheed Missiles and Space Co. Huntsville, AL, United States)
Date Acquired
September 4, 2013
Publication Date
February 1, 1981
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
LMSC-HREC-TR-D784066
NASA-CR-161646
Report Number: LMSC-HREC-TR-D784066
Report Number: NASA-CR-161646
Accession Number
81N18087
Funding Number(s)
CONTRACT_GRANT: NAS8-33976
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available