1443. Synthesis and Optimization of Large Space Structures for Orbital Transfer
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Paper
1443. Synthesis and Optimization of Large Space Structures for Orbital Transfer. 1981.
Abstract
A computerized analytical procedure is described for synthesizing and then size-optimizing a
large space structure to handle accelerations required for transferring it from the Shuttle at
low earth-orbit (LEO) to geosynchronous orbit (GEO). This paper examines the effects of
alternative construction materials, onboard equipment masses, mass fraction in structural
joints, and selected minimum gauges in truss members. The analysis accounts for the payload
and volume limitations of the Shuttle cargo bay.
