Publication Date:
2019-07-13
Description:
Traditionally, a fixed base modal test has been performed as a means of verifying the coupled loads math model for Space Shuttle flight payloads. An alternate method, a free-free configured payload using mass loaded boundary conditions, is presented as a means of verifying the coupled loads model of the ASTRO-1 flight payload. This method allows evaluation of the influence of local load paths into the frequency range of the free-free test. The method is cost effective and does not contaminate the modal test results with fixture coupled modes or boundary condition uncertainties. This paper describes the mass additive modal test technique as applied to the Space Shuttle ASTRO-1 flight payload.
Keywords:
LAUNCH VEHICLES AND SPACE VEHICLES
Type:
International Modal Analysis Conference; Feb 01, 1988 - Feb 04, 1988; Kissimmee, FL; United States
Format:
text
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