Thermal control arrangements for a geosynchronous spacecraft

Heat exchange – With vehicle feature

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165904, 244158R, 244163, F28D 1500, G05D 2300

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active

053721837

ABSTRACT:
A spacecraft adapted for operation in a low inclination angle earth orbit comprises north, south, east and west panels defining a spacecraft interior volume. The north and south panels are oppositely disposed with respect to each other and the east and west panels are oppositely disposed with respect to each other. The spacecraft interior volume generally and preferably lacks structural elements that substantially restrict thermal radiation among the panels. The north and south panels, to which spacecraft equipment is usually mounted, each include conductive heat pipes for reducing the temperature differences across each panel. The exterior surfaces of the north, south, east and west panels have a covering, preferably of optical solar reflectors (OSRs), for radiating thermal energy therefrom, wherein the OSRs have a solar absorptivity that is substantially less than their thermal emissivity. The interior surfaces of the north, south, east and west panels have a covering for effectively radiating thermal energy between and among the panels across the interior volume.

REFERENCES:
patent: 3205937 (1965-09-01), Shyffer
patent: 3422636 (1969-01-01), Fuschillo et al.
patent: 3548930 (1970-12-01), Byrd
patent: 3603530 (1971-09-01), Easton et al.
patent: 3671286 (1972-06-01), Fischell
patent: 3744478 (1973-07-01), Gopin
patent: 3749156 (1973-07-01), Fletcher et al.
patent: 4009851 (1977-03-01), Cable
patent: 4161212 (1979-07-01), Hightower
patent: 4162701 (1979-07-01), Ollendorf
patent: 4603731 (1986-08-01), Olsen
patent: 4669685 (1987-06-01), Dalby
patent: 4682744 (1987-07-01), Gounder
patent: 4687048 (1967-08-01), Edelstein et al.
patent: 4706740 (1987-11-01), Mahefkey
patent: 4738304 (1988-04-01), Chalmers et al.
patent: 4830097 (1989-05-01), Tanzer
patent: 4880050 (1989-11-01), Nakamura et al.
patent: 5036905 (1991-08-01), Eninger et al.
patent: 5069274 (1991-12-01), Haslett et al.
GE AstroSpace Telstar 4 Spacecraft Description Sheet. This sheet become available no earlier than Oct. 1990.
GE AstroSpace Satcom C-1 Spacecraft Descriptive Sheet. No date.
GE Proposal Document, Telstar 4 Satellite, pp. 2-125 to 2-134 of vol. 2, Oct. 1988.
GE Proposal Document, Telstar 4 Satellite, pp. 3.5-1 to 3.5-5, 3.5-15 to 3.5-22 and 3.5-30 to 3.5-32 of vol. 3, Book 2, Oct. 1988.
GE Proposal Document, GE American Communications SATCOM H1 Satellite, vol. 2, pp. 9.1-1 to 9.1-6, 9.6-1 to 9.6-6, and 9.8-5 to 9.8-6, issued 17 Sep. 1990.
Technical Handbook AED M-2170, Section IX, Thermal Control, "Programming and Control Handbook for RCA Satcom Spacecraft," pp. IX-1 through IX-19 (circa Mar. 1975).
The Missions Operations Plan RCA Americom handbook, AED R-4117F, pp. 3-5 through 3-15, issued Nov. 17, 1975.
"RCA SATCOM 1 & 2 Flight History and End-of-Life Testing" article, pp. 1-6 and The Life and Times of SATCOMS 1 and 2, pp. 1-3, 19 and 20, AIAA-86-0708-CP (circa Sep. 1986).
Telesat ANIK-B Communications Satellite Spacecraft Operations Manual, issued Jun. 2, 1978, Section VII.A., Thermal Control, pp. VII-1, -3, -10, and II-11.
"The Effects of Electrostatic Discharge Phenomena on Telesat's Domestic Communications Satellites," by P. N. Wadham, No. 87-TE-008, pp. 25-1 through 25-9, Jun. 1986.

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