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JSAT-8

JSAT Orders 7TH Satellite from BSS

JCSAT-8 satellite animation (Neg#: 00PR-01209)

Customer JSAT Corporation
Tokyo, Japan
Spacecraft Boeing 601
Launch
  Vehicle
  Site
March 28, 2002
Ariane
Kourou, French Guiana
Orbital Slot 154° E Longitude
Contract life 11 years

Boeing Satellite Systems (BSS) and JSAT signed an agreement in April 2000 for a Boeing 601 model satellite. Known as JCSAT-8, the spacecraft is the seventh satellite ordered by JSAT from BSS.

JCSAT-8 replaces JCSAT-2 at the orbital slot of 154 degrees East longitude. This will enable the new satellite to provide coverage to Japan, East Asia, Australia and Hawaii. The satellite was launched on March 28, 2002 aboard an Ariane 4 rocket.

Artist rendering of JCSAT 8 satellite shown stowed and deployed.
Stowed (left); In Orbit (right)

JCSAT-8 carries 16 Ku-band transponders, each with 120 watts provided by traveling-wave tube amplifiers (TWTAs), and 16 C-band transponders, each with 34 watts provided by solid-state power amplifiers (SSPAs).

JSAT has been a BSS customer since the 1980s. The first two spacecraft ordered were 393 model spinning satellites. JCSAT-3 through 6 are all Boeing 601 bodystabilized models. These satellites have at least twice the power of the spinning versions. BSS also built JSAT's master control station in Yokohama and the backup station in Gunma.

JCSAT-8 is the latest in the Boeing 601 satellite line. As of January 2002, customers around the world have ordered more than 80 Boeing 601s, making the Boeing 601 the most-purchased commercial communications satellite model. Like all 601s, the new satellite will consist of a cube-shaped center payload section, with the solar panel wings extending from the north and south sides, and an antenna array.

Boeing Satellite Systems is the world's leading manufacturer of commercial communications satellites, and is also a major provider of space systems, satellites, and payloads for national defense, science and environmental applications.

JCSAT-8 SPECIFICATIONS

PAYLOAD
Ku-band 16 transponders
120-w TWTAs
C-band 16 transponders
34-w SSPAs
POWER
Solar Beginning of life

   End of life

   Panels
4.1 kW

3.7 kW (Equinox)
3.4 kW (Solstice)
2 wings each w/3 panels of silicon solar cells
Batteries 27-cell NiH, 160-Ahr
PROPULSION
Liquid apogee motor 110 lbf (490 N)
Stationkeeping thrusters
   N-S (bipropellant)
   E-W (bipropellant)
   Aft (bipropellant)

4 x 5 lbf (22 N)
4 x 5 lbf (22 N)
4 x 5 lbf (22 N)
DIMENSIONS
In orbit L, solar arrays: 68.8 ft (21 m)
W, antennas: 24.9 ft (7.6 m)
Stowed H: 14 ft (4.3 m)
W: 8.8 ft x 11.7 ft
(2.7 m x 3.6 m)
Mass
   Launch
   In orbit
   (beginning of life)

5735 lb (2600 kg)
3530 lb (1600 kg)
ANTENNAS
1 85-in (2.2m) Ku-band dual-gridded shaped relector
1 85-in (2.2m) C-band dual-gridded shaped reflector

Public Relations
Boeing
P.O. Box 92919 (S10/S323)
Los Angeles, CA 90009
USA
(310) 364-6363
www.boeing.com/satellite

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