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Galaxy VII

Dual-Payload Satellite for Galaxy® System

Galaxy VII satellite animation (Neg#: 91-03928)

Customer PanAmSat Corp., Greenwich, CT
Spacecraft Hughes 601
Launch
   Date
   Vehicle
   Site

Oct. 27, 1992
Ariane 42P
Kourou, French Guiana
Orbital Slot 91° W
Contract life 12 years

The Galaxy® VII satellite brought C-band and Ku-band services together for the first time on the same spacecraft for American customers of PanAmSat Corporation.

The spacecraft is a version of the three-axis, body-stabilized Hughes 601 model built by Hughes Space and Communications Company (HSC) in El Segundo, Calif. In October 2000, the company became Boeing Satellite Systems, Inc. PanAmSat is the world's leading commercial provider of satellite-based communications services. The company operates a global network of 19 satellites supported by PanAmSat professionals on five continents. These resources enable PanAmSat to provide video and telecommunications services to hundreds of customers worldwide.

Galaxy VII was launched Oct. 27, 1992, aboard an Ariane 42P rocket from Kourou, French Guiana. With 24 C-band and 24 Ku-band transponders, the new satellite offers double the capacity of the satellite it replaced, which was a Hughes 376 spin-stabilized model also built by Hughes Space and Communications.

Galaxy VII was configured to provide coverage to all 50 United States plus the Caribbean basin, with a signal strength of 36 dBW in C-band and 45 dBW in Ku-band across the contiguous United States.

Artist rendering of Galaxy VII satellite shown stowed and deployed.
Stowed (left); In Orbit (right)
All Hughes 601-now the Boeing 601-spacecraft use the same basic bus design, allowing the company to realize efficiencies gained by production volume, tooling investments, and quantity buys. The model was introduced in 1987 to meet anticipated requirements for high-power, multiple-payload satellites for such applications as television relay, direct-to-home broadcasting, private business networks, and mobile communications.

The Boeing 601 body is composed of two modules. The first contains the primary bus structure that carries all launch vehicle loads and contains the propulsion subsystem, bus electronics, and battery packs. The second payload module is a structure of honeycomb shelves that hold the communications equipment, electronics, and isothermal heat pipes. Reflectors, antenna feeds, and solar arrays mount directly to the payload module, and antenna configurations can be placed on three faces of the bus. This modular approach allows work to proceed in parallel, thereby shortening the manufacturing schedule and test time.

Boeing Satellite Systems is the world's leading manufacturer of commercial communications satellites. It is also a major supplier of spacecraft for communications and space exploration to the U.S. government and builds weather satellites for the United States and Japan.

GALAXY VII SPECIFICATIONS

PAYLOAD
C-band 24 active (6 spare)
16-w SSPAs
Ku-band 24 active (6 spare)
50-w TWTAs
POWER
Solar
   Beginning of life
   End of life
   Panels

5.4 kw
4.3 kw
2 solar wings, each w/4
panels of K7 silicon cells
Batteries 32-cell NiH
PROPULSION
Liquid apogee motor 110 lbf (490N)
Stationkeeping thrusters
   (all bipropellant)
12 x 5 lbf (22N)
DIMENSIONS
In orbit L, solar arrays: 86 ft (26.2 m)
W, antennas: 24 ft (7.3 m)
Stowed H: 9 ft 8 in (3 m)
W: 8 ft 10 in x 11 ft 9 in
(2.7 m x 3.6 m)
Mass
   Launch
   In orbit
   (beginning of life)

6634 lb (3009 kg)
3710 lb (1683 kg)
ANTENNAS
2 ovals, 8 ft x 6 ft (2.4 m x 1.8 m),
one each for C-band and Ku-band;
dual-gridded for vertical and horizontal
polarization
HSC 980035_026/1000/3-99