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JCSAT-11

From Wikipedia, the free encyclopedia
JCSAT-11
Mission typeCommunication
OperatorSKY Perfect JSAT Group
COSPAR ID2007-F03[1]
Spacecraft properties
SpacecraftJCSAT-11
BusA2100AX
ManufacturerLockheed Martin
Launch mass4,007 kg (8,834 lb)
Dimensions27 m × 9 m (89 ft × 30 ft) with solar panels and antennas deployed.
Start of mission
Launch date22:43:10, September 5, 2007 (UTC) (2007-09-05T22:43:10Z)
RocketProton-M/Briz-M
Launch siteBaikonurSite 200/39
ContractorILS
End of mission
DestroyedLaunch failure
Transponders
Band18 × 27 Mhz and 12 × 36 MHzKu band
12 × 36 MHzC band
Bandwidth1,350 MHz
TWTA powerKu band 127 W
C band 48 W

JCSAT-11, was ageostationarycommunications satellite ordered byJSAT Corporation (nowSKY Perfect JSAT Group) which was designed and manufactured byLockheed Martin on theA2100 platform. The satellite was designated to be used as an on-orbit, but was lost on launch failure.[2]

Satellite description

[edit]

The spacecraft was designed and manufactured byLockheed Martin on theA2100AXsatellite bus. It had a launch mass of 4,007 kg (8,834 lb) and a 15-year design life. A near copy ofJCSAT-3A, it was to be used as an on orbit spare.[2] As most satellites based on the A2100 platform, it uses a 460 N (100 lbf)LEROS-1CLAE fororbit raising.[2] Its solar panels span 27 m (89 ft) when fully deployed and, with its antennas in fully extended configuration it is 9 m (30 ft) wide.[3]

Its payload is composed of eighteen 27 MHz and twelve 36 MHzKu band plus twelveC bandtransponders, for a total bandwidth of 1,350 MHz.[4] Itshigh-power amplifiers had an output power of 127 Watts on Ku band and 48 Watts on C band.[3]

History

[edit]

On October 3, 2005, JSAT ordered anA2100AX based satellite fromLockheed Martin,JCSAT-11. It would be an almost copy ofJCSAT-3A, with aC band andKu band payload. It was expected to be launched in 2007 to act as a backup for the whole JSAT fleet.[5]

The almost 19-year streak of successful JCSAT launches was ended when aProton-M/Briz-M failed to orbit JCSAT-11 on September 5, 2007. A damaged pyro firing cable on the interstage truss prevented the second stage from controlling its direction, and the rocket and its payload crashed into the Kazakhstan steppes.[6] Being lucky in misfortune, JCSAT-11 was simply an on-orbit backup and thus it had no operational impact on the fleet.[2]

The same day of the launch failure, JSAT placed an order with Lockheed for an identical replacement,JCSAT-12, for launch in 2009.[2] On September 19, 2007, they closed a deal withArianespace for a launch slot with an Ariane 5 for its launch.[7]

References

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  1. ^McDowell, Jonathan."Proton". Retrieved2016-08-10.
  2. ^abcdeKrebs, Gunter Dirk (2016-04-21)."JCSat 10, 11, 12 (JCSat 3A, RA)".Gunter's Space Page. Retrieved2016-07-20.
  3. ^ab"JCSAT-RA".SKY Perfect JSAT Group. Archived fromthe original on August 18, 2016. RetrievedAugust 9, 2016.
  4. ^"Who we are". SSKY Perfect JSAT Group. 2012-08-03. Archived fromthe original(PDF) on 2016-09-08. Retrieved2016-08-02.
  5. ^"JSAT Corporation Awards Lockheed Martin Contract For Third A2100 Satellite".Icaa.eu.Lockheed Martin Space Systems. October 3, 2005. Retrieved2016-08-05.
  6. ^Zak, Anatoly (September 12, 2007)."Proton/JCSAT-11 launch failure". Russian Space Web. Retrieved2016-08-05.
  7. ^"Arianespace to Launch Japanese Satellite JCSAT-12".Defense-aerospace.com.Arianespace. September 19, 2007. Archived fromthe original on 2021-11-21. Retrieved2016-08-05.
JCSAT satellites
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Operational designations
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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).
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