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| subject: | 4\21 ILS Proton to Launch AMC-9 Satellite |
This Echo is READ ONLY ! NO Un-Authorized Messages Please! ~~~~~~~~~~~~~~~~~~~~~~~~ ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~ 21 Apr 2003 ILS Proton to Launch AMC-9 Satellite Media Advisory Payload: AMC-9 Spacebus 3000B3 platform Separated mass: approx. 4,100 kg (9,039 lbs) Launch Vehicle: Proton K/Breeze M Weight at liftoff: 691,272 kg (1.5 million lbs), including payload Height: 61 m (200 ft) Launch Date: April 29, 2003 (Baikonur) April 28, 2003 (GMT, U.S.) Launch Window Opens: 4:15 a.m. Baikonur 22:15 GMT 6:15 p.m. EDT Launch Site: Baikonur Cosmodrome, Kazakhstan Launch Pad 39 End User: SES AMERICOM, Princeton, N.J. Part of SES GLOBAL family of companies Satellite Manufacturer: Alcatel Space, Cannes, France Launch Vehicle Manufacturer: Khrunichev State Research and Production Space Center, Moscow Launch Services Provider: International Launch Services, McLean, Va. Satellite Use: High-power communications satellite operating at C- and Ku-band to expand digital television broadcasting, data transmission and telecommunications services to North America Satellite Statistics: 1st delivery-in-orbit launch for Alcatel by ILS 8th Alcatel satellite launched by ILS 5th ILS launch for AMERICOM Orbital location: 72 degrees West longitude Anticipated service life of 15 years Mission Profile: The Proton launch vehicle will inject the satellite into geosynchronous transfer orbit, using a five-burn Breeze M mission design. The first three stages of the Proton will use a standard ascent trajectory to place the Breeze M fourth stage, with the satellite, into a suborbital trajectory, from which the Breeze M will place itself and the spacecraft into a circular parking orbit of 180 km (112 miles), inclined at 51.6 degrees. Then the satellite will be propelled to its transfer orbit by additional burns of the Breeze M. Following separation from the Breeze M, the spacecraft will perform a series of liquid apogee engine burns to raise perigee, lower inclination and circularize the orbit at the geostationary altitude of 36,000 km (22,300 miles). Spacecraft Separation: Approximately 8 hours, 55 minutes after liftoff ILS Mission Statistics: 300th Proton launch 1st Proton mission this year 2nd ILS mission this year 27th ILS mission on Proton since formation of the U.S.-Russian joint venture in 1995 2nd ILS launch in a month - END OF FILE - ========== @Message posted automagically by IMTHINGS POST 1.30 ---* Origin: SpaceBase(tm) Pt 1 -14.4- Van BC Canada 604-473-9358 (1:153/719.1) SEEN-BY: 633/267 270 @PATH: 153/719 715 7715 140/1 106/2000 633/267 |
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