Actions for Pressure signatures for a .00053 scale model of the Saturn 5-Apollo launch vehicle with simulated exhaust plumes

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Pressure signatures for a .00053 scale model of the Saturn 5-Apollo launch vehicle with simulated exhaust plumes

Author
Mendoza, J. P.
Published
Jul 1, 1973.
Physical Description
1 electronic document
Additional Creators
Hicks, R. M.
Online Version

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Restrictions on Access
Unclassified, Unlimited, Publicly available.
Free-to-read Unrestricted online access
Summary
Wind tunnel pressure signatures are presented for 10 Mach numbers over a range from 3.01 to 7.29 for a .00053-scale model of the Saturn 5 Apollo launch vehicle complete with escape tower and solid body simulated exhaust plumes for each Mach number. The effect of simulated plume length on the wind tunnel pressure signature was investigated at Mach 4.01. An analysis of the error incurred by extrapolating pressure signatures having strong shock waves by weak shock procedures is presented.
Other Subject(s)
Collection
NASA Technical Reports Server (NTRS) Collection.
Note
Document ID: 19730022098.
Accession ID: 73N30830.
NASA-TM-X-62129.
Terms of Use and Reproduction
No Copyright.
View MARC record | catkey: 15747900