Transient Dynamic Response of Orbiting Space Stations

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Report Number: FDL TDR 64-25
Author(s): Tai, C. L., Andrew, L. V., Loh, M. M. H., Kamrath, P. C.
Corporate Author(s): North American Aviation, Incorporated
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1965-02
Pages: 369
Contract: AF 33(657)-10219
DoD Project: 1370
DoD Task: 137008
Identifier: AD0613081

The dynamic responses of thirteen selected configurations, composed of two to three inter-connected compartments and subjected to various applied disturbances, were investigated first by approximate exploratory analyses to determine the significant configurations for space stations and the relative significance of transient inputs to each configuration. Then detailed analyses of ten selected combinations of configurations and forcing functions were carried out in depth. In addition, because of the unique dynamic response problems of the cableconnected configuration, the Y-configuration and the Hconfiguration of space stations subjected to the influence of the gravitational gradient and elastic effects, separate detailed analyses of these configurations were conducted.

Provenance: Lockheed Martin Missiles & Fire Control

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