Names | JCSAT-2A (March 2002 onward) JCSAT-8 (April 2000 to March 2002) |
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Mission type | Communications |
Operator | SKY Perfect JSAT Group |
COSPAR ID | 2002-015A |
SATCAT no. | 27399 |
Website | JSAT official page |
Mission duration | 11 years (planned) |
Spacecraft properties | |
Spacecraft | JCSAT-2A |
Bus | BSS-601 |
Manufacturer | Boeing Satellite Systems |
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 | 29 March 2002. 01:29 UTC |
Rocket | Ariane 44L H10-3 |
Launch site | Centre Spatial Guyanais, ELA-2 |
Contractor | Arianespace |
Orbital parameters | |
Reference system | Geocentric orbit |
Regime | Geostationary orbit |
Longitude | 154° East |
Transponders | |
Band | Ku-band: 16 × 57 MHz C-band: 11 × 36 MHz + 5 × 54 MHz |
Bandwidth | 1,578 MHz |
Coverage area | Japan, East Asia, Australia, Hawaii |
TWTA power | Ku-band: 120 watts C-band: 34 watts |
JSAT← JCSAT-110JCSAT-5A → |
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 Satellite Systems 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.
Satellite description
The spacecraft was designed and manufactured by Boeing Satellite Systems 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. 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).
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. Its high-power amplifiers had an output power of 120 watts on Ku-band and 34 watts on C-band.
The Ku-band footprint covers only Japan, while the C-band beams cover Japan, East Asia, Australia and Hawaii.
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.
An Ariane 44L successfully launched JCSAT-8 on 29 March 2002 at 01:29 UTC from Centre Spatial Guyanais. Once successfully deployed, it was renamed JCSAT-2A.
References
- ^ "Display: JCSAT 8 2002-015A". NASA. 10 February 2021. Retrieved 18 March 2021. This article incorporates text from this source, which is in the public domain.
- ^ "JCSat 8 (JCSat 2A)". Gunter's Space Page. 11 December 2017. Retrieved 18 March 2021.
- "JCSat 2A (JCSat 8)". Satbeams. Retrieved 26 July 2016.
- ^ "JCSAT-2A". SKY Perfect JSAT. Archived from the original on 17 November 2016. Retrieved 9 August 2016.
- ^ "Launch Kit V149" (PDF) (in French). Arianespace. 18 March 2002. Archived from the original (PDF) on 11 April 2004. Retrieved 8 September 2016.
- "Who we are?". SKY Perfect JSAT. 3 August 2012. Archived from the original on 8 September 2016. Retrieved 2 August 2016.
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