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S-2 stage 1/25 scale model base region thermal environment test. Volume 1: Test results, comparison with theory and flight dataA 1/25 scale model S-2 stage base region thermal environment test is presented. Analytical results are included which reflect the effect of engine operating conditions, model scale, turbo-pump exhaust gas injection on base region thermal environment. Comparisons are made between full scale flight data, model test data, and analytical results. The report is prepared in two volumes. The description of analytical predictions and comparisons with flight data are presented. Tabulation of the test data is provided.
Document ID
19730021151
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Sadunas, J. A. (Rockwell International Corp. Downey, CA, United States)
French, E. P. (Rockwell International Corp. Downey, CA, United States)
Sexton, H. (Rockwell International Corp. Downey, CA, United States)
Date Acquired
September 2, 2013
Publication Date
May 1, 1973
Subject Category
Space Vehicles
Report/Patent Number
NASA-CR-129009
SD73-SA-0061-VOL-1
Accession Number
73N29883
Funding Number(s)
CONTRACT_GRANT: NAS7-200
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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