Spacecraft structure for orbital assembly and servicing

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

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244161, 244172, B64G 140, B64G 164

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active

049645960

ABSTRACT:
A spacecraft structure for orbital assembly and servicing includes a payload module, a propulsion module and a bus module each of these modules includes attachement means for separately attching to the cargo bay of the Shuttle directly and via planar cradles. The bus module includes module docking and latching fittings at each end and matching locking and latching fittings at one end of each of said payload and propulsion modules. The bus module includes sectionalized assemblies forming a matrix of identical cavities adapted to receive orbital replacement submodules that allow easy replacement of equipment in orbit by an astronaut.

REFERENCES:
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patent: 3467891 (1969-09-01), Mogle
patent: 3788259 (1974-01-01), Colin
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patent: 4298178 (1981-11-01), Hujsak
patent: 4471926 (1984-09-01), Steel, III
patent: 4607815 (1986-08-01), Turci et al.
Runge, "Space Tug/Spacecraft/Module Exchanger", Mechanism and Machine Theory, 1977, vol. 12, No. 5, pp. 451-462.
Fairchild, "On-Orbit Spacecraft Servicing", Brochure delivered AIAA Tech Display Conference, 1983.
"Assembly and Maintenance of Space Platforms"by Sved, published in the Journal of the British Interplanetary Society, July 1985.
Paper No. AAS 85-398; AAS/AIAA Astrodynamics Specialist Conference; "Eureca Concept and its Potential Evolution Within the Space Station Era"; by R. Mory, Aug. 12-15, 1985, pp. 17 and 18.

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