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Launch site:
Baikonur, Launch pad no. 45/2 (45°56'24.33"N, 63°39'19.32"E)
Launch date:December 1, 2009
The launch time is:
3 : 00 : 00 Baikonur 01.12.2009
0 : 00 : 00 Moscow Local 01.12.2009
21 : 00 : 00 UTC Nov 30, 2009
4 : 00 : 00 p.m. EST Nov 30, 2009
[eventTimer]2009-11-30 21:00:00?before|after;%dd% Days %hh% Hours %mm% Minutes %ss% Seconds %c%[/eventTimer] Intelsat 15 launch
Payload: Intelsat 15 communications satellite
Spacecraft: Intelsat 15
Manufacturer: Orbital Sciences Corporation
Mission Description
The Intelsat 15 (IS-15) satellite being manufactured for Intelsat will replace Intelsat 709 currently positioned at 85 degrees East Longitude. The high power Ku-band payload will provide video and data services for the Middle East, Indian Ocean Regions and Russia. Based on Orbital's START spacecraft bus, IS-15 will produce 4.6 kW of payload power and feature two 2.3 meter dual-grid deployable reflectors as well as one 1.4 meter deck-mounted antenna.
Performances
Spacecraft
Launch Mass|2,550 kg (5,622 lb.)
Solar Arrays|Four panels per array, UTJ Gallium Arsenide cells
Stabilization|3-axis stabilized; zero momentum system
Propulsion|Liquid bi-propellant transfer orbit system; Monopropellant (hydrazine) on-orbit system
Batteries|Two >4840 W-Hr capacity Li-Ion batteries
Mission Life|15 years (fueled for 16 years)
Orbit|85 degrees East Longitude
Payload
Frequency|Ku-band
Repeater|22 active transponders with 30-for-22 redundant TWTA's
Antenna|Two 2.3 m deployable dual-grid reflectors; one 1.4 m deck-mounted antenna
Coverage Contour Maps
Middle East EIRP
Russia Beam
Russia and adjacent countries coverage, detailed
Launcher: Zenit-3SLБ with DM-SLБ upper stage
Manufacturers: Yuzhmash (A.M. Makarov Yuzhny Machine-Building Plant) - Ukraine, RKK Energia - Russia.
In place of the Boeing-made fairing used on Sea Launch, the Zenit-3SLB adopts a 4-meter fairing made by NPO Lavochkin. It is in current production and has been flight-proven with the Block DM.
The vehicle's reliability statistics according to http://www.spacelaunchreport.com/reliability2009.txt:
Code:
================================================================
Vehicle Successes/Tries Realzd Pred Consc. Last Dates
Rate Rate* Succes Fail
================================================================
Zenit 3SLB/DMSLB 2 3 .67 .60 2(B) 4/28/08 2008-
Mission Profile
From our launch site at the Baikonur Space Center in Kazakhstan, a Zenit-3SLB launch vehicle will lift the 2,484 kg (5,477 lbs) Intelsat 15 communications satellite to geosynchronous transfer orbit, on its way to a final orbital position of 85 degrees East Longitude. The first stage will operate for two-and-a-half minutes and then separate, followed by the jettison of the payload fairing three minutes later. After a six-minute burn, the second stage will separate from the Block DM-SLB upper stage. The Block DM will then begin the first of three burns, taking the spacecraft to a stable parking orbit. After a brief second burn, the upper stage will coast with the spacecraft for five hours, after which a third burn will inject the spacecraft into a geosynchronous transit orbit. Eleven minutes later, the spacecraft will separate from the upper stage. Following spacecraft separation, ground stations in Hartebeesthoek, South Africa, and Perth, Australia, will be tracking the satellite to acquire its first signals from orbit.
Launch Timeline
L= 0 : 00 : 00|Liftoff
L + 0 : 02 : 29|Stage 1 Separation
L + 0 : 05 : 16|Payload Fairing Jettison
L + 0 : 08 : 31|Stage 2 Separation
L + 0 : 08 : 41|Block DM 1st Burn Ignition
L + 1 : 20 : 14|Block DM 2nd Burn Ignition
L + 6 : 14 : 03|Block DM 3rd Burn Ignition
L + 6 : 26 : 42|Spacecraft Separation
L + 6 : 30 : 00|Spacecraft Acquisition (estimated time)
Zenit-3SLB's parts drop zones
References
http://www.federalspace.ru
http://tvroscosmos.ru
http://www.sea-launch.com
http://www.orbital.com
http://forum.nasaspaceflight.com
http://www.orion-express.ru
http://www.spacelaunchreport.com
http://weatherbug.com
http://www.good-stuff.co.uk/suntimes/sunmap.php
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