JCSAT-2A
| Names | JCSAT-8 (Apr 2000 to Mar 2002) JCSAT-2A (Mar 2002 onward) |
|---|---|
| Mission type | Communication |
| Operator | SKY Perfect JSAT Group |
| COSPAR ID | 2002-015A[1] |
| SATCAT no. | 27399[2] |
| Website | JSAT Official Page |
| Spacecraft properties | |
| Spacecraft | JCSAT-8 |
| Bus | HS-601 |
| Manufacturer | Hughes |
| Launch mass | 2,460 kg (5,420 lb) |
| Dimensions | 21 m × 7.6 m × 4.6 m (69 ft × 25 ft × 15 ft) with solar panels and antennas deployed. |
| Power | 3.7 kW |
| Start of mission | |
| Launch date | 01:29:00, March 29, 2002 (UTC)[1] |
| Rocket | Ariane 44L |
| Launch site | GSC ELA-2 |
| Contractor | Arianespace |
| Orbital parameters | |
| Regime | GEO |
| Longitude | 154°East |
| Transponders | |
| Band | Ku band: 16 × 57 Mhz C band: 11 × 36 MHz + 5 × 54 MHz |
| Bandwidth | 1,578 MHz |
| TWTA power | Ku band 120 W C band 34 W |
JCSAT-2A, known as JCSAT-8 before launch, is a geostationary communications satellite operated by SKY Perfect JSAT Group (JSAT) which was designed and manufactured by Boeing on the BSS-601 platform. It has Ku band and C band payload and was used to replace JCSAT-2 at the 154°East longitude. It covers Japan, East Asia, Australia and Hawaii.[3][2][4]
Satellite description
The spacecraft was designed and manufactured by Boeing on the BSS-601 satellite bus. It had a launch mass of 2,460 kg (5,420 lb) a power production of 3.7 kW and an 11-year design life.[3] Stowed for launch it measured 3.6 m × 2.7 m × 4.3 m (11.8 ft × 8.9 ft × 14.1 ft), with its solar panels and antennas deployed it measured 21 m × 4.3 m × 7.6 m (69 ft × 14 ft × 25 ft).[4][5]
Its payload is composed of sixteen 57 MHz Ku band plus eleven 36 MHz and five 54 MHz C band transponders, for a total bandwidth of 1,578 MHz.[6] Its high power amplifiers had an output power of 120 Watts on Ku band and 34 Watts on C band.[4][5]
The Ku band footprint covers only Japan, while the C band beams cover Japan, East Asia, Australia and Hawaii.[4]
History
In April 2000, JSAT ordered JCSAT-8 from Boeing (which had acquired the HS-601 business from Hughes), to replace JCSAT-2 at the 154° East slot. It would provide coverage to Japan, East Asia, Australia and Hawaii.[3]
An Ariane 44L successfully launched JCSAT-8 on March 29, 2002 at 01:29 UTC from Guiana Space Centre. Once successfully deployed, it was renamed JCSAT-2A.[3]
References
- ^ a b "JCSAT 8". NASA Space Science Data Coordinated Archive. 27 April 2016. Retrieved 2016-08-04.
- ^ a b "JCSat 2A (JCSat 8)". Satbeams. Retrieved 26 July 2016.
- ^ a b c d Krebs, Gunter Dirk (2016-04-21). "JCSat 8 (JCSat 2A)". Gunter's Space Page. Retrieved 2016-07-20.
- ^ a b c d "JCSAT-2A". SKY Perfect JSAT Group. Retrieved August 9, 2016.
- ^ a b "Launch Kit V-149" (PDF) (in French). Arianespace. March 18, 2002. Archived from the original (PDF) on 2004-04-11. Retrieved 2016-09-08.
- ^ "Who we are" (PDF). SSKY Perfect JSAT Group. 2012-08-03. Retrieved 2016-08-02.
