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A survey of payload integration methodsSeveral full-scale and short-cut methods for analyzing a booster/payload system are presented. Two full-scale techniques are considered: (1) a technique that uses a restrained payload together with a free-booster model, the latter being augmented with residual mass and stiffness correction and (2) a technique that uses a restrained payload and booster model. Both techniques determine the 'modal modes', which require the solution of a system eigenvalue problem; the loads usually are then determined via an acceleration approach. A brief description is given of a number of short-cut methods which are of special interest to Shuttle payload design: structural modification, base drive, and interface impedance methods. Directions for further research and development are suggested.
Document ID
19840066714
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Engels, R. C.
(Tennessee, University Tullahoma, TN, United States)
Craig, R. R., Jr.
(Texas, University Austin, TX, United States)
Harcrow, H. W.
(Martin Marietta Aerospace Denver, CO, United States)
Date Acquired
August 12, 2013
Publication Date
October 1, 1984
Publication Information
Publication: Journal of Spacecraft and Rockets
Volume: 21
ISSN: 0002-4650
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
84A49501
Funding Number(s)
CONTRACT_GRANT: NAS8-33556
Distribution Limits
Public
Copyright
Other

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