Another SUPERBIRD Joins the Flock
| Customer | Space Communications Corporation |
|---|---|
| Spacecraft | Boeing 601 |
| Launch Date Vehicle Site |
April 15, 2004 Atlas IIAS Cape Canaveral AS, Florida |
| Orbital Slot | 158° E Longitude |
| Mission life | Approx. 13 years |
Space Communications Corporation (SCC), a Japanese satellite communications service company, ordered SUPERBIRD-6, a Boeing 601 communications satellite, from Boeing Satellite Systems in September 2001. It is the third Boeing satellite to be built for SCC. SUPERBIRD-6 was launched April 15, 2004 on an Atlas IIAS launch vehicle from Cape Canaveral AS, Florida, however it failed to reach the proper orbit due to underperformance of the booster.
SUPERBIRD-6, was slated for an orbital slot at 158.0 degrees East longitude, and would have provided business telecommunication services to Japan in Ku-Band and Ka-Band and an additional Ka-Band services using a Steerable Spot Beam. The satellite has a payload of 23 active Ku-Band transponders and four Ka-Band transponders.
The first SUPERBIRD spacecraft built by Boeing Satellite Systems, SUPERBIRD-C, was launched in July 1997. Then, SUPERBIRD-4(B2) was launched in February 2000.
Mitsubishi Corporation (MC), Mitsubishi Electric Corporation (MELCO), and other Mitsubishi Group Companies established Space Communications Corporation of Tokyo, Japan in 1985.
SUPERBIRD is the name of the series of high-performance communications satellites owned and operated by SCC. SCC now operates four communications satellites named SUPERBIRD-A, B2, C, and D at four orbital slots, by which SCC is providing stable and high quality telecommunication services to a wide range of customers.
Boeing Satellite Systems is major provider of space systems, communications satellites, and payloads for national defense, science, environmental and commercial applications.
SUPERBIRD-6 SPECIFICATIONS
| Ku-band Ka-band |
23 active Ku-Band transponders Four active Ka-Band transponders |
|---|
| Solar End of life Panels |
4 Panel Array 4378 W (June solstice) Populated with Silicon Solar Cells |
|---|---|
| Batteries | 200 Ahr Nickel Hydrogen composed of 29 cells |
| Liquid apogee motor | 445N (100 lbf) |
|---|---|
| Stationkeeping thrusters Axial (bipropellant) E-W (bipropellant) |
22N (5lbf) 22N (5lbf) |
| Receive | East, 85" Single Shaped Surface Ka-Band West. 85" Dual Gridded Shaped Ku-Band Nadir, 47" Single Shaped Surface Ka-Band Steerable Spot |
|---|---|
| Transmit | East, 85" Single Shaped Surface Ka-Band West, 85" Dual Gridded Shaped Ku-Band Nadir, 47" Single Shaped Surface Ka-Band Steerable Spot |
| In orbit | Approximately 84.8ft x 24.6ft x 14.8ft (26.2m x 7.5m x 4.5m) |
|---|---|
| Stowed | Approximately 14.8ft x 11.5ft x 11.5ft (4.5m x 3.5m x 3.5m) |
| Mass Launch at Separation In orbit (beginning of life) End of life |
Approximately 6834 lbs. (3100 kg) Approximately 3367 lbs. (1528 kg) Approximately 3256 lbs. (1477 kg) |
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