NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Space Shuttle payload trunnion interface verification test and correlation with fixed based responsesAn interface verification test (IFVT) in the free-free condition was conducted to verify that the constrained modes of a mass simulator had the same frequencies as the Hubble Space Telescope, for which it was designed. Landing tests were performed in which the mass simulator was mounted on its trunnions inside a container onboard an aircraft. Its acceleration response was adequately measured, and the anticipated constrained natural frequencies based on the IFVT were confirmed. The first test updated the model to predict the fixed based modes, and the second verified the test's capacity to characterize the structure. The IFVT is shown to generate information which permits accurate modeling of the constrained structure, without requiring the traditional fixed-based modal test.
Document ID
19910050861
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Blair, Mark A.
(Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Vadlamudi, Nagarjuna
(Lockheed Missiles and Space Co., Inc. Sunnyvale, CA, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1990
Subject Category
Spacecraft Design, Testing And Performance
Meeting Information
Meeting: International Modal Analysis Conference
Location: Kissimmee, FL
Country: United States
Start Date: January 29, 1990
End Date: February 1, 1990
Accession Number
91A35484
Funding Number(s)
CONTRACT_GRANT: NAS8-32697
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available