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Contents

   



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1 Satellite description  





2 History  





3 See also  





4 References  














JCSAT-110







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From Wikipedia, the free encyclopedia
 

(Redirected from Superbird-5)

JCSAT-110
NamesN-SAT 110 (Nov 1998 to Oct 2000)
JCSAT-7 (Nov 1998 to Oct 2000)
JCSAT-110 (Oct 2000 onward)
Superbird-5 (Nov 1998 to Oct 2000)
Superbird-D (Oct 2000 to Oct 2008)
Mission typeCommunications
OperatorSKY Perfect JSAT Group
COSPAR ID2000-060A [1]
SATCAT no.26559
WebsiteJSAT official page
Mission duration13 years (planned)
Spacecraft properties
SpacecraftJCSAT-110
Spacecraft typeJCSAT
BusA2100-AX
ManufacturerLockheed Martin Space
Launch mass3,531 kg (7,785 lb)
Dry mass1,669 kg (3,680 lb)
Power8.3 kW
Start of mission
Launch date6 October 2000, 23:00 UTC
RocketAriane 42L H10-3
Launch siteCentre Spatial Guyanais, ELA-2
ContractorArianespace
Orbital parameters
Reference systemGeocentric orbit
RegimeGeostationary orbit
Longitude110° East
Transponders
Band24Ku-band × 36 MHz transponders
Bandwidth864 MHz
Coverage areaJapan
TWTA power120 watts
 

JCSAT-110, also known as N-SAT 110, JCSAT-7, Superbird-5 and Superbird-D, is a Japanese geostationary communications satellite which was operated by JSAT Corporation and Space Communications Corporation until both companies merged into SKY Perfect JSAT Group in 2008. It is positioned in geostationary orbit at a longitude of 110° East, from where it is used to provide communications services to Japan.[2][3][4]

Satellite description

[edit]

The spacecraft was designed and manufactured by Lockheed Martin on the A2100-AX satellite bus. It had a launch mass of 3,531 kg (7,785 lb) with a dry mass of 1,669 kg (3,680 lb) and a 13-year design life. As most satellites based on the A2100-AX platform, it uses a 460 N (100 lbf) LEROS-1C liquid apogee engine (LAE) for orbit raising.

When stowed for launch, the satellite was 6 m (20 ft) high. Its dual wing solar panels gave a power generation capability of 8.3 kW at the end of its design life, with a span of 26.4 m (87 ft) when deployed.[5][6] With antennas deployed, its width was 8.3 m (27 ft).[2]

Its payload is composed of twenty-four 36 MHz Ku-band transponders with a TWTA output power of 120 watts per channel. With its total bandwidth of 864 GHz, it is used primarily for multi-channel pay per view business.[7][5][8]

History

[edit]

In September 1997, both JCSAT and Space Communications Corporation (SCC) had requested the 110° East position.[9] The Japanese government made both companies share the 110° East position, and thus they both made a joint order on 20 November 1998 for N-SAT 110 from Lockheed Martin.[9][10] JCSAT used the JCSAT-7 designation for this satellite, while SCC used Superbird-5.[5]

On 6 October 2000 at 23:00 UTC, an Ariane-42L H10-3 successfully launched N-SAT 110 to a geostationary transfer orbit from Centre Spatial Guyanais ELA-2.[11] One hour later, at 00:04 UTC, on 7 October 2000, the first signals from the satellite were successfully received from the Australia ground station.[12] On 14 October 2000, at around 03:00 UTC, N-SAT 110 reached the geostationary orbit.[13] Once it was put into orbit, it was renamed as JCSAT-110 by JCSAT and Superbird-D by SCC.[5]

On 1 October 2008, JSAT Corporation and Space Communications Corporation merged into SKY Perfect JSAT Group, and the satellite was known simply as JCSAT-110.[7]

See also

[edit]

References

[edit]
  1. ^ "Display: N-SAT 110 2000-060A". NASA. 10 February 2021. Retrieved 18 March 2021.
  • ^ a b "N-SAT-110". SKY Perfect JSAT. Archived from the original on 8 September 2016. Retrieved 8 September 2016.
  • ^ "Satellite Fleet JSAT". SKY Perfect JSAT. Archived from the original on 3 September 2016. Retrieved 26 August 2016.
  • ^ "N-SAT 110". Satbeams. Retrieved 8 September 2016.
  • ^ a b c d "N-SAT 110 (JCSat 110, JCSat 7, Superbird 5 (D))". Gunter's Space Page. 21 April 2016. Retrieved 20 July 2016.
  • ^ "Launch Kit V-133" (PDF) (in French). Arianespace. 29 September 2000. Archived from the original (PDF) on 11 April 2004. Retrieved 6 September 2016.
  • ^ a b "Who we are?". SKY Perfect JSAT. 3 August 2012. Archived from the original on 8 September 2016. Retrieved 2 August 2016.
  • ^ "Main specifications of SUPERBIRD-D". Space Communications Corporation. Archived from the original on 4 June 2004. Retrieved 26 August 2016.
  • ^ a b "Superbird". Global Security. Retrieved 28 July 2016.
  • ^ "Lockheed Martin Selected to Build A2100 Satellite to Serve Japanese Telecommunications Market". prnewswire.com. Lockheed Martin. 20 November 1998. Archived from the original on 8 September 2016. Retrieved 8 September 2016.
  • ^ "Display: N-SAT 110 2000-060A". NASA. 10 February 2021. Retrieved 18 March 2021.
  • ^ "Lockheed Martin Selected to Build A2100 Satellite to Serve Japanese Telecommunications Market". Lockheed Martin. 6 October 2000. Archived from the original on 18 December 2007. Retrieved 8 September 2016.
  • ^ McDowell, Jonathan. "Index". Geostationary Orbit Catalog. Jonathan's Space Report. Archived from the original on 8 September 2016. Retrieved 8 September 2016.

  • Retrieved from "https://en.wikipedia.org/w/index.php?title=JCSAT-110&oldid=1143088650"

    Categories: 
    Communications satellites of Japan
    Spacecraft launched in 2000
    Satellites using the A2100 bus
    2000 in Japan
    Hidden categories: 
    CS1 French-language sources (fr)
    Use American English from March 2021
    All Wikipedia articles written in American English
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    This page was last edited on 5 March 2023, at 21:45 (UTC).

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