A method is described for placing a large, STS-compatible platform on orbit utilizing a construction method employing both deployable and erectable structures. A multifunctional mechanism is used for deployable structures and an on-orbit assembly is used for erectable structures. Also analyses are discussed which assess the thermal distortion of a simple open truss and a more complex truss.
Structural/thermal considerations for design of large space platform structures
01.01.1978
Aufsatz (Konferenz)
Keine Angabe
Englisch
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