Intelsat 6
Part of the Intelsat program
At the time, the Intelsat 6 series were the largest commercial spacecraft ever built. The series were also the first commericial satellites to employ Satellite Switched/Time Division Multiple Access (SS/TDMA) techniques.
Spacecraft
Based on Hughes 393 bus. Spin stabilized with despun antenna. Hydrazine propulsion system. Passive thermal control. Telescoping dual-cylinder structure with deployed antennas. Body mounted solar cells generate 2250 W (EOL). Solar drums are each about 6m tall.
Payload
38 (plus 12 backup) C-Band and 10 (plus 4 backup) Ku-Band transponders. 120,000 telephone calls and 3 color TV broadcasts simultaneously. SS/TDMA (Satellite-Switched Time Division Multiple Access) techniques used.
Country of Origin | International |
Customer/User | ITSO |
Manufacturer(s) | Hughes |
Size | Cylinder: 11.8 m high, 3.6 m diameter |
Orbit | Geosynchronous |
Design Life | 13 years |
Launch Facts
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Name | Int'l Desig. | Date | Site | Vehicle | Orbit | Mass(kg) |
Notes |
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Intelsat 6 F-2 | 1989-087A | 10/27/89 | Kourou | Ariane 44L | GEO | 4215 |
24.5 deg E |
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Intelsat 6 F-3 | 1990-021A | 3/14/90 | ESMC | Titan 3 | LEO | 4215 |
2nd stage separation failure; unusable orbit |
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Intelsat 6 F-4 | 1990-056A | 6/23/90 | ESMC | Titan 3 | GEO | 4215 |
International communications; 63 deg E |
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Intelsat 6 F-5 | 1991-055A | 8/14/91 | Kourou | Ariane 44L | GEO | 4296 |
International communications; 14.5 deg W |
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Intelsat 6 F-1 | 1991-075A | 10/29/91 | Kourou | Ariane 44L | GEO | 4330 |
International communications; 27.5 deg W |
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