NASA Logo

NTRS

NTRS - NASA Technical Reports Server

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

Back to Results
Space Shuttle Plume and Plume Impingement StudyThe extent of the influence of the propulsion system exhaust plumes on the vehicle performance and control characteristics is a complex function of vehicle geometry, propulsion system geometry, engine operating conditions and vehicle flight trajectory were investigated. Analytical support of the plume technology test program was directed at the two latter problem areas: (1) definition of the full-scale exhaust plume characteristics, (2) application of appropriate similarity parameters; and (3) analysis of wind tunnel test data. Verification of the two-phase plume and plume impingement models was directed toward the definition of the full-scale exhaust plume characteristics and the separation motor impingement problem.
Document ID
19770010202
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Tevepaugh, J. A.
(Lockheed Missiles and Space Co. Huntsville, AL, United States)
Penny, M. M.
(Lockheed Missiles and Space Co. Huntsville, AL, United States)
Date Acquired
September 3, 2013
Publication Date
March 1, 1977
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
LMSC-HREC-TR-D497190
NASA-CR-151202
Report Number: LMSC-HREC-TR-D497190
Report Number: NASA-CR-151202
Accession Number
77N17145
Funding Number(s)
CONTRACT_GRANT: NAS9-14845
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available