NASA Logo

NTRS

NTRS - NASA Technical Reports Server

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

Back to Results
Preliminary sonic boom correlation of predicted and measured levels for STS-1 entryA preliminary analysis correlating peaks from sonic boom pressure signatures recorded during the descent trajectory of the Orbiter Columbia, which landed in the dry lake bed at Edwards Air Force Base (EAFB), California, with measured wind tunnel signatures extrapolated from flight altitudes to the ground has been made for Mach numbers ranging from 1.3 to 6. The flight pressure signatures were recorded by microphones positioned at ground level near the groundtrack, whereas the wind tunnel signatures were measured during a test of a 0.0041-scale model Orbiter. The agreement between overpressure estimates based on wind tunnel data using preliminary flight trajectory data and oscillograph traces from ground measurements appears reasonable at this time for the range of Mach numbers considered. More detailed studies using final flight trajectory data and digitized ground measured data will be performed.
Document ID
19820013160
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Garcia, F., Jr.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Morrison, K. M.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Jones, J. H.
(NASA Marshall Space Flight Center)
Henderson, H. R.
(NASA Langley Res. Center)
Date Acquired
September 4, 2013
Publication Date
February 1, 1982
Subject Category
Acoustics
Report/Patent Number
NAS 1.15:58242
NASA-TM-58242
S-511
Report Number: NAS 1.15:58242
Report Number: NASA-TM-58242
Report Number: S-511
Accession Number
82N21034
Funding Number(s)
PROJECT: RTOP 953-36-00-00-72
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available