AsiaSat 3 [Boeing BSS]
Asia Satellite Telecommunications Co. Ltd. (AsiaSat) selected Hughes Space and Communications International, Inc., in February, 1996 to build a Hughes HS-601HP (for high-power) satellite, provide a launch vehicle, and perform ground station upgrades. The satellite, AsiaSat 3, was to serve Asia and neighboring regions.
The body-stabilized AsiaSat 3 was to be used primarily for television distribution and telecommunications services throughout Asia, the Middle East, Australasia, and the Commonwealth of Independent States, with multiple spot beams for selected areas. It carried 28 active C-band transponders and 16 active Ku-band transponders. The C-band transponders were powered by 55 watt traveling wave tube amplifiers (TWTAs). The Ku-band transponders used 138 watt TWTAs.
As a high-power Hughes HS-601HP model, AsiaSat 3 was to generate up to 9900 Watts using two sun-tracking four-panel solar wings covered with gallium arsenide solar cells. A 29-cell nickel-hydrogen battery was to provide full power to the spacecraft during eclipse operations. The satellite was to use a bipropellant propulsion system for stationkeeping.
AsiaSat 3 had two 107-inch diameter Gregorian shaped-surface antennas. One of these antennas, to operate in C-band and to provide broad-area coverage of Asia and Australasia, was mounted on the east side of the satellite. The other antenna, to operate in Ku-band and to provide focused-area coverage of East Asia, was mounted on the west side.
Focused area coverage of South Asia was to be provided by a 50-inch-diameter, dual-gridded shaped reflector operating in the Ku-band. A 40-inch-diameter Ku-band steerable spot-beam antenna was to provide the spacecraft with the ability to direct 5-degree coverage of any area on the Earth's surface visible to AsiaSat 3 from its orbit location. Both of these antennas were mounted on the nadir side of the spacecraft.
AsiaSat 3 was launched on 25 December 1997, aboard a Proton-K Blok-DM3 rocket from the Baikonur Cosmodrome in Kazakhstan. The launch failed, however, in the fourth stage of the launch vehicle's second burn. Designed to last 110 seconds, it cut off prematurely after 1 second. As a result, AsiaSat 3 never reached geosynchronous orbit and was declared a total loss by its insurers. The satellite was transferred under the designation HGS-1 to Hughes Global Services, Inc., with an agreement to share any profits with the insurers. This satellite was salvaged by a unique lunar flyby maneuvre and sent to a inclined geosynchronous satellite orbit at the 152º W location with about half of its designed life time remaining. After the satellite was in a stable orbit, the satellite was commanded to release its solar panels which had been stowed during takeoff and maneuvering. Of the satellite's two solar panels only one released, and it became apparent that a tether was not operating correctly on board, which scientists attributed to heating and cooling cycles during the satellites operating in ranges not designed to while traveling to orbit. In early 1999, PanAmSat acquired the HGS-1 satellite. Subsequently, PanAmSat requested, and was granted, authority to drift the satellite, now referred to as PAS-22, into the 60º West location. It was finally deactivated in July 2002, and moved to a graveyard orbit.
In March 1998, AsiaSat ordered a replacement satellite from Hughes. Designated AsiaSat 3S, the new satellite is a replica of AsiaSat 3. This one was successfully launched on a Proton-K Blok-DM3 rocket.
HGS 1 reportedly is experiencing some problems with its batteries. One of its 30 battery cells has been reported lost.
|Nation:||Hong Kong → China|
|Type / Application:||Communication|
|Operator:||Asia Satellite Telecommunications Company (Hughes Global Satellite, PanAmSat for #3)|
|Contractors:||Hughes → Boeing|
|Equipment:||28 C-band, 16 Ku-band transponders|
|Power:||2 deployable solar arrays, batteries|
|Mass:||3400 kg (#3), 3465 kg (#3S)|
|AsiaSat 3 → HGS 1 → PAS 22||1997-086A||24.12.1997||TB LC-81/23||P||Proton-K Blok-DM3|
|AsiaSat 3S||1999-013A||21.03.1999||TB LC-81/23||Proton-K Blok-DM3|