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Sonic boom measurement test plan for Space Shuttle STS-5 launchSonic booms measurements are obtained at key locations within the focus region and the lateral attenuation rate during ascent is determined in order to assess the validity of existing capability to predict the extent of focus boom area, the number of booms within the various zones (focus and nonfocus regions), the overpressures, and focus factors. The sonic boom focus region, consists of a region on the ground (in the form of an inverted 'horseshoe' pattern) in which higher than nominal overpressures can occur.
Document ID
19830010142
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Henderson, H. R.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
November 1, 1982
Subject Category
Acoustics
Report/Patent Number
NASA-TM-85225
NAS 1.15:85225
Report Number: NASA-TM-85225
Report Number: NAS 1.15:85225
Accession Number
83N18413
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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