Movatterモバイル変換


[0]ホーム

URL:


Jump to content
WikipediaThe Free Encyclopedia
Search

AsiaSat 2

From Wikipedia, the free encyclopedia
AsiaSat communications satellite

AsiaSat 2
NamesAMOS-5i
Mission typeCommunications
OperatorAsiaSat (1995–2009, 2012)
Spacecom (2009–2011)
COSPAR ID1995-064AEdit this at Wikidata
SATCATno.23723
Websitehttps://www.asiasat.com
Mission duration13 years (planned)
16 years (achieved)
Spacecraft properties
SpacecraftAsiaSat-2
Spacecraft typeAS-7000
BusLockheed Martin AS-7000
ManufacturerLockheed Martin Astro Space
Launch mass3,379 kg (7,449 lb)
Start of mission
Launch date28 November 1995,
11:30:05UTC
RocketLong March 2E /FG-46
Launch siteXichang,LA-2
ContractorCGWIC
Entered serviceJanuary 1996
End of mission
DisposalGraveyard orbit
DeactivatedMay 2012
Orbital parameters
Reference systemGeocentric orbit
RegimeGeostationary orbit
Longitude100.5° East (1995–2009)
17° East (2009–2010)
120° East (2012)
Transponders
Band34transponders:
26C-band
8Ku-band
Coverage areaAsia,Pacific Ocean
← AMOS-3
AMOS-5 →

AsiaSat 2 was aHong Kongcommunications satellite, which was owned, and was initially operated, by the Hong Kong–basedAsia Satellite Telecommunications Company. It was positioned ingeostationary orbit at a longitude of 17° East of theGreenwich Meridian, on lease toSpacecom.[1] It spent most of its operational life at 100.5° East,[2] from where it was used to providefixed satellite services, including broadcasting, audio and data transmission, toAsia and thePacific Ocean.[3]

Satellite description

[edit]

AsiaSat 2 was built byAstro Space, which by the time of its launch had become part ofLockheed Martin. It is based on theAS-7000satellite bus. At launch, it had a mass of 3,379 kg (7,449 lb),[3] and a design life of thirteen years. It carries twenty sixC-band and eightKu-bandtransponders.[2]

Launch

[edit]

The launch of AsiaSat 2 was contracted to theChina Great Wall Industry Corporation (CGWIC), and used aLong March 2Elaunch vehicle with aFG-46 upper stage.[4] It was the maiden flight of the FG-46,[4] and the first Chinese launch since theApstar 2 failure, which killed a number of villagers in January 1995.[5] The launch was conducted fromXichang Launch Area 2 (LA-2) at theXichang Satellite Launch Centre at 11:30:05UTC on 28 November 1995.[6] The launch had previously been delayed twice, first from December 1994 due to the failure ofTelstar 402, which was based on the same satellite bus as AsiaSat 2, and subsequently whilst the Apstar 2 launch failure was investigated.[4]

Since theLong March 2E launch vehicle had experienced two failures in five launches, AsiaSat 2 had to pay a 27% premium forsatellite insurance instead of the usual 17–20%. Although the satellite was delivered to the correct orbit, the launch was a partial failure. Excessive acceleration during the launch caused a misalignment of the antenna feed horns on the Ku-band transponders, reducing the satellite's coverage area.[7] AsiaSat filed an insurance claim for US$58 million.[8]

AMOS-5i

[edit]

AsiaSat 2 was replaced byAsiaSat 5 in 2009,[9] and in September 2009 it was leased toIsraeli operatorSpacecom Ltd. It was subsequently moved to a longitude of 17° East, and in January 2010 it began operations for Spacecom, who refer to it as AMOS-5i. Spacecom intended to operate it untilAMOS-5 was launched in 2011,[1] however during a stationkeeping manoeuvre in August 2010 they discovered that it was carrying less fuel than they had expected, meaning that it would have to be retired before the launch of its replacement.[10]

See also

[edit]

References

[edit]
  1. ^abde Selding, Peter B. (29 January 2010)."Spacecom Leases Satellite, Inks Launch Deal with SpaceX". SpaceNews. Archived fromthe original on 2 February 2013. Retrieved5 February 2010.
  2. ^ab"AsiaSat 2".Satellite Fleet. AsiaSat. Archived fromthe original on 7 July 2011. Retrieved4 August 2009.
  3. ^abKrebs, Gunter (21 July 2019)."AsiaSat 2". Gunter's Space Page. Retrieved2 May 2021.
  4. ^abcHarland, David M; Lorenz, Ralph D. (2005).Space Systems Failures (2006 ed.). Chichester: Springer-Praxis.ISBN 0-387-21519-0.
  5. ^Wade, Mark."CZ". Encyclopedia Astronautica. Archived fromthe original on 7 September 2008. Retrieved4 August 2009.
  6. ^McDowell, Jonathan (14 March 2021)."Launch Log". Jonathan's Space Page. Retrieved2 May 2021.
  7. ^"CZ-2E Space Launch Vehicle". GlobalSecurity.org.
  8. ^"Ku Transponder Shortfall Prompts AsiaSat Claim". Aviation Week & Space Technology. 23 September 1996.
  9. ^"AsiaSat 5". AsiaSat. Retrieved2 May 2021.
  10. ^Zeno, Lior (9 August 2010)."Israeli satellite Amos-5i about to run out of fuel".Haaretz.com. Archived fromthe original on 11 August 2010. Retrieved2 May 2021.
AsiaSat satellites
Future spacecraft initalics.
Earth observation
Communication and engineering
Data relay satellite system
Satellite navigation system
Astronomical observation
Lunar exploration
Planetary exploration
Microsatellites
Future spacecraft initalics.
January
February
March
April
May
June
July
August
September
October
November
December
Launches are separated by dots ( • ), payloads by commas ( , ), multiple names for the same satellite by slashes ( / ).
Crewed flights are underlined. Launch failures are marked with the † sign. Payloads deployed from other spacecraft are (enclosed in parentheses).
Retrieved from "https://en.wikipedia.org/w/index.php?title=AsiaSat_2&oldid=1245416208"
Categories:
Hidden categories:

[8]ページ先頭

©2009-2025 Movatter.jp