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Skylab vibroacoustic test programVibroacoustic testing was performed on the orbital workshop dynamic test article and the payload assembly, the two major elements of the Skylab payload. The testing was conducted on each of the Skylab elements separately in the reverberation chamber at the Johnson Space Center. The two test configurations were high fidelity flight article simulations. The testing was conducted in two phases; in the first phase, acoustic tests were performed at levels simulating the lift-off and atmospheric flight acoustic criteria. In the second phase, low frequency sinusoidal vibration tests were conducted to obtain modal response data. The objectives of the Skylab vibroacoustic test program were to: verify the vibration design and test criteria; qualify selected flight components to the vibroacoustic criteria; and verify analytical models used for dynamic load analyses. This paper describes the vibroacoustic testing and discusses the results.
Document ID
19740059310
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Jewell, R. E.
(NASA Marshall Space Flight Center Structural Dynamics Div., Huntsville, Ala., United States)
Date Acquired
August 7, 2013
Publication Date
August 1, 1974
Subject Category
Structural Mechanics
Report/Patent Number
AAS PAPER 74-106
Meeting Information
Meeting: Annual Meeting
Location: Los Angeles, CA
Start Date: August 20, 1974
End Date: August 22, 1974
Sponsors: American Astronautical Society
Accession Number
74A42060
Distribution Limits
Public
Copyright
Other

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