Intelsat-5A
Intelsat-5A |
The Intelsat 5A series is very similar to the Intelsat 5 series. Modifications include a larger communications payload with internal weight savings to accommodate the additional mass. 3-axis stabilized to 0.4 deg with momentum wheels. Hydrazine propulsion system. Passive thermal control. Dual solar arrays provide 1800 W (BOL). Nickel hydrogen batteries.
The payload consists of 26 C-Band and 6 Ku-Band transponders for 15000 voice circuits
and 2 TV channels.
| Nation: | International, Netherlands (NSS) |
|---|---|
| Type / Application: | Communication |
| Operator: | Intelsat / New Skies (NSS) / Columbia |
| Contractors: | Ford |
| Equipment: | 26 C-band transponders, 6 Ku-band transponders |
| Configuration: | |
| Propulsion: | Star-37XF |
| Lifetime: | 9 years |
| Mass: | |
| Orbit: | GEO |
| Satellite | Date | LS | Launcher | Remarks: | |
|---|---|---|---|---|---|
| Intelsat-5A 10 -> Intelsat 510 | 23.03.1985 | CC LC-36B | Atlas-G Centaur-D1AR | ||
| Intelsat-5A 11 -> Intelsat 511 | 30.06.1985 | CC LC-36B | Atlas-G Centaur-D1AR | ||
| Intelsat-5A 12 -> Intelsat 512 | 28.09.1985 | CC LC-36B | Atlas-G Centaur-D1AR | ||
| Intelsat-5A 13 -> Intelsat 513 -> NSS 513 | 17.05.1988 | Ko ELA-1 | Ariane-2 | ||
| Intelsat-5A 14 | 031.05.1986 | Ko ELA-1 | F | Ariane-2 | |
| Intelsat-5A 15 -> Intelsat 515 -> Columbia 515 -> 515 | 27.01.1989 | Ko ELA-1 | Ariane-2 |
Last update: 27.09.2009
Contact: gunter.krebs@skyrocket.de
© Gunter Dirk Krebs