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A comparison of acoustic and random vibration testing of spacecraftBefore selecting the most suitable testing technique in a particular case, it has to be considered which of the two methods duplicates better the distribution of vibration responses to be expected during the actual launch phase. An investigation is conducted of the case of a large, low density spacecraft launched by a vehicle which produces significant acoustic noise and transmits relatively little vibration through the mechanical path provided by the vehicle structure in the area of the spacecraft interface. Criteria for vibration-acoustic equivalence are discussed along with tests conducted with the Synchronous Meteorological Satellite, the Radio Astronomy Explorer, and the Orbiting Geophysical Spacecraft. The investigation indicates that the vibration test is generally a poor substitute for an acoustic study.-
Document ID
19740053255
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Bangs, W. F.
(NASA Goddard Space Flight Center Applied Dynamics Section, Greenbelt, Md., United States)
Date Acquired
August 7, 2013
Publication Date
January 1, 1974
Subject Category
Space Vehicles
Meeting Information
Meeting: Annual Meeting on the Cost effectiveness in the environmental sciences
Location: Washington, DC
Start Date: April 28, 1974
End Date: May 1, 1974
Accession Number
74A36005
Distribution Limits
Public
Copyright
Other

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