ADVISORY/ILS Reschedules AMC-9 Satellite Launch for June 7.News Editors/Assignment Desks/High-Tech Writers ADVISORY...for Friday Friday: see Sabbath; week. Friday young Indian rescued by Crusoe and kept as servant and companion. [Br. Lit.: Robinson Crusoe] See : Servant (June June: see month. 6) --(BUSINESS WIRE)
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: June 7, 2003 (Baikonur)
June 6, 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
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
-- 16th in SES AMERICOM constellation
-- Orbital location: 85 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).
Target Orbit
at Separation: Apogee: 35,786 km
Perigee: 6,661 km
Inclination: 17.54 degrees
Spacecraft Separation: Approximately 8 hours, 55 minutes after
liftoff
ILS Mission Statistics: -- 300th Proton launch
-- 1st ILS Proton mission this year
-- 3rd ILS mission this year
-- 27th ILS mission on Proton since formation
of the U.S.-Russian joint venture in 1995
-- 3rd ILS launch in two months
Live Broadcast
in U.S.: AMC-4, 101 degrees West, analog, transponder
22/C-band, downlink 4140MHz (H); digital,
transponder 21/Ku-band, downlink 12120 MHz
(V), FEC 3/4, 30 Msyms. Test signals start at
5:30 p.m. June 6 EDT
More Information: Live webcast and general mission information
are available on the ILS web site at
www.ilslaunch.com. Launch status updates are
available on the ILS U.S. domestic Launch
Hotline at 1-800-852-4980.
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