NASA NTRS · 19930049891
Spacecraft on-orbit coupled loads analysis
Abstract
A method is presented for coupled loads analysis of on-orbit spacecraft systems. Discrete models are coupled then reduced using the Craig-Bampton technique. Coupled system transient response is determined as well as substructure interface forces and center-of-gravity accelerations. Typical results are presented for a spacecraft system having three components and being subjected to rocket motor thrust.
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Tinker, Michael L.. 1993-01-01. Spacecraft on-orbit coupled loads analysis. https://ntrs.nasa.gov/citations/19930049891
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