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Sonic-boom measurements in the focus region during the ascent of Apollo 17Sonic-boom pressure signatures recorded during the ascent phase of Apollo 17 are presented. The measurements were obtained onboard six U.S. Navy ships positioned along the ground track of the spacecraft vehicle in the area of expected focus resulting from the flight path and acceleration of the vehicle. Tracings of the measured signatures are presented along with values of the maximum positive overpressure, positive impulse, signature duration, and bowshock rise time. Also included are brief descriptions of the ships and their location, the deployment of the sonic-boom instrumentation, flight profiles and operating conditions for the launch vehicle and spacecraft, surface-weather and sea-state information at the measuring sites, and high-altitude weather information for the general measurement areas. Comparisons of the measured and predicted sonic-boom overpressures for the Apollo 17 mission are presented. The measured data are also compared with data from the Apollo 15 and 16 missions and data from flight test programs of various aircraft.
Document ID
19750005520
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Henderson, H. R.
(NASA Langley Research Center Hampton, VA, United States)
Hilton, D. A.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 3, 2013
Publication Date
December 1, 1974
Subject Category
Acoustics
Report/Patent Number
L-9649
NASA-TN-D-7806
Report Number: L-9649
Report Number: NASA-TN-D-7806
Accession Number
75N13592
Funding Number(s)
PROJECT: RTOP 743-04-31-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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