Printer Friendly
The Free Library
19,573,962 articles and books
Member login
User name  
Password 
 
Join us Forgot password?

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.
COPYRIGHT 2003 Business Wire
No portion of this article can be reproduced without the express written permission from the copyright holder.
Copyright 2003, Gale Group. All rights reserved. Gale Group is a Thomson Corporation Company.

 Reader Opinion

Title:

Comment:



 

Article Details
Printer friendly Cite/link Email Feedback
Publication:Business Wire
Date:Jun 3, 2003
Words:450
Previous Article:S&P:Eur'n Invstmt-Grade Issuance Despite Cred Quality.
Next Article:NewsStand Launches Enhanced Reader; New Version Significantly Improves Digital Reading Experience.



Related Articles
SES AMERICOM Orders 2 Launches From International Launch Services.
ADVISORY/ILS Proton to Launch AMC-9 Satellite.
ADVISORY/ILS Reschedules Proton Launch Of AMC-9 Satellite.
ILS Proton Successfully Launches AMC-9 Satellite; 300th Mission Flown by Proton Vehicle.
ILS to Launch SES AMERICOM Satellite for Broadband Services Next Year.
SES AMERICOM Commits to Proton Launch for AMC-15; Hybrid Spacecraft Designated for DTH Broadband & Video Services.
ADVISORY/ILS To Launch AMC-10 Satellite on Atlas.
ILS Successfully Orbits AMC-10 Satellite; 1st Atlas Mission in Busy Launch Year.
CORRECTING AND REPLACING ILS Adds 5th AMERICOM Satellite to 2004 Launch Schedule.
Double Success: ILS Launches Payloads with Atlas and Proton on Same Day; Overlapping Missions Demonstrate Unmatched Launch Tempo.

Terms of use | Copyright © 2012 Farlex, Inc. | Feedback | For webmasters | Submit articles