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Launch Failure
Liftoff Time (GMT)
22:43:09
Wednesday September 5, 2007
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The first stage functioned correctly, but an anomaly of the second stage caused the engines to stop at H0+135". The launcher continued its flight on a ballistic trajectory until an altitude of 76km and then crashed at H0+330" at approximately 40km in the south-west of Dzhezkazgan, in the center of Kazakhstan.
Lockheed Martin has been awarded a contract by JSAT Corporation of Japan to build its next geostationary telecommunications satellite, designated JCSAT-10, which will provide communications services throughout Japan and Asia following its scheduled launch in 2006. Financial terms were not disclosed. JCSAT-10 will be a hybrid satellite, equipped with Ku-band high-power transponders and C-band medium-power transponders, and will be located at 128 degrees East longitude. The spacecraft is based on the award-winning A2100AXS platform manufactured by Lockheed Martin Commercial Space Systems (LMCSS), Newtown, Pa. After becoming operational, the satellite is referred by the designator JCSat 3A. Lockheed Martin has been awarded a contract by JSAT Corporation (JSAT) of Japan in October 2005 to build its next geostationary telecommunications satellite, designated JCSAT-11. JCSAT-11 was to be reserved entirely in orbit as a backup satellite for other JCSAT satellites following its scheduled launch in 2007. Financial terms were not disclosed. JCSAT-11 was lost in a launch failure.
Geostationary Transfer Orbit
1 Payload
4,007 kilograms
Manufacturer
KhrunichevPrice
$65.00 million
Rocket
Height: 58.18m
Payload to Orbit
LEO: 21,000 kg
GTO: 6,900 kg
Liftoff Thrust
10,027 Kilonewtons
Fairing
Diameter: 4.35m
Height: 15.26m
Stages
4
17th
Mission
3rd
Mission of 2007
40th
Orbital launch attempt