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SUPERBIRD-6

Another SUPERBIRD Joins the Flock

SUPERBIRD-6 satellite animation (Neg#: 02PR-01600)

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, today known as Boeing Space & Intelligence 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.

Artist rendering of Superbird 6 satellite shown stowed and deployed.
Stowed (left); In Orbit (right)

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

PAYLOAD
Ku-band Ka-band
23 active Ku-Band transponders Four active Ka-Band transponders
POWER
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
PROPULSION
Liquid apogee motor 445N (100 lbf)
Stationkeeping thrusters
   Axial (bipropellant)
   E-W (bipropellant)

22N (5lbf)
22N (5lbf)
ANTENNAS
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
DIMENSIONS
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)
020035_015/1000/03-02