![Quicklook](../headers/ql.gif)
Intelsat 4A
Part of the Intelsat program
Intelsat 4A satellites increased satellite capacity to 7250 voice circuits or 2 TV channels.
Spacecraft
Spin stabilized with a despun antenna structure. Hydrazine propulsion system. Passive thermal control. Body mounted solar cells.
Payload
Twenty transponders. Multiple access. 7250 voice circuits or 2 TV channels.
Country of Origin | International |
Customer/User | ITSO |
Manufacturer(s) | Hughes |
Size | Cylinder: 2.8 m long (6.8 m w/antenna), 2.4 m diameter |
Orbit | F1: GEO over Atlantic / F2: GEO over Atlantic / F3: GEO over Indian Ocean / F4: GEO over Atlantic / F6: GEO |
Design Life | 7 years |
Launch Facts
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Name | Int'l Desig. | Date | Site | Vehicle | Orbit | Mass(kg) |
Notes |
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Intelsat 4A F-1 | 1975-091A | 9/26/75 | ESMC | Atlas Centaur | GEO | 1500 |
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Intelsat 4A F-2 | 1976-010A | 1/30/76 | ESMC | Atlas Centaur | GEO | 1500 |
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Intelsat 4A F-4 | 1977-041A | 5/26/77 | ESMC | Atlas Centaur | GEO | 1500 |
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Intelsat 4A | none | 9/29/77 | ESMC | Atlas Centaur | FTO | 1500 |
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Intelsat 4A F-3 | 1978-002A | 1/7/78 | ESMC | Atlas Centaur | GEO | 1511 |
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Intelsat 4A F-6 | 1978-035A | 3/31/78 | ESMC | Atlas Centaur | GEO | 826 |
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Information in The Mission and Spacecraft Library is provided without
warranty or guarantee. USE AT YOUR OWN RISK.
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