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BATTERY THERMAL DESIGN AND PERFORMANCE IN EUROPEAN GEO-SATELLITE PROGRAMS MBB/ERNO Raumfahrttechnik GmbH, 2800 Bremen, West Germany

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Konzok, H.-G, author.
Conference Name:
Intersociety Conference on Environmental Systems (1987-07-13 : Seattle, Washington, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1987
Summary:
This paper outlines and compares the thermal control design and thermal accommodation of the batteries of various European communications satellites, viz the ESA spacecraft OTS, ECS, MCS, and Olympus, the German, French and British national programs: DFS-Kopernikus, TV-SAT, TDF1 and Skynet IV, and the Inmarsat II maritime comms satellite.The performance of these battery thermal control systems is discussed versus their specific design features using flight results or analytical predictions as available.A conclusion is drawn with respect to achievements versus investments and an outlook is attempted on development trends
Notes:
Vendor supplied data
Publisher Number:
871484
Access Restriction:
Restricted for use by site license

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