Survivable satellite bus structural frame

Aeronautics and astronautics – Spacecraft – Spacecraft formation – orbit – or interplanetary path

Patent

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Details

428116, B64G 150, B32B 312

Patent

active

043974341

ABSTRACT:
A three-sided prism shaped structure including upper and lower graphite/epoxy honeycomb sandwich decks spaced by rectangular graphite/epoxy longerons and braces, all of which are attached by using machined aluminum fittings. A graphite/epoxy sandwich panel and cone assembly is bonded to one side of the structure for mounting a space sextant therein. Aluminum equipment panels are attached to the other two sides. The bus structure is manufactured in accordance with available procedures for fabricating graphite/epoxy composite material which is the primary structural material.

REFERENCES:
patent: 4016022 (1977-04-01), Browning et al.
patent: 4136846 (1979-01-01), Brault
patent: 4259821 (1981-04-01), Bush

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