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HS-393

Boeing 393
Manufacturer Boeing Satellite Development Center
Country of origin United States
Applications Communications satellite
Specifications
Spacecraft type Spin-stabilized
Design life 8 years
Launch mass 2.2 to 2.5 t (2.4 to 2.8 tons)
Dimensions Diameter: 3.7 m (12 ft)
Height (stowed): 3.4 m (11 ft)
Height (deployed): 10 m (33 ft)
Power 2 to 2.2 kWatts
Batteries 2 × 38Ah NiH2 batteries
Regime Geostationary orbit
Production
Status Retired
Built 3
On order 3
Launched 3
Retired 3
First launch JCSAT-1 March 6, 1989
Last launch SBS 6, October 12, 1990
Related spacecraft
Derived from HS-376
← HS-376 Boeing 601

The Hughes 393 (sometimes referred to as the HS-393 is a communications satellite bus introduced in 1985 by Hughes Space and Communications Company. It was a spin-stabilized bus that had twice as much power as the HS-376 platform.

The satellite bus was designed and manufactured by Hughes. It had a launch mass of 2.2 to 2.5 t (2.4 to 2.8 tons), a mass of 1.35 to 1.5 t (1.49 to 1.65 tons) after reaching geostationary orbit and an 8-year design life. When stowed for launch, its dimensions were 3.4 m (11 ft) in height and 3.7 m (12 ft) in diameter. With its solar panels fully extended its height was 10 m (33 ft).

Its power system generated approximately 2,350 Watts of power at BOL and 2,200 at end of life, thanks to two cylindrical solar panels. These panels used K7 and K4-3/4 solar cells and were more than twice the number than on the HS-376 The bottom panel was retracted around the body and top panel for launch, and extended downwards for operation. It also had a two 38Ah NiH2 batteries.

Its propulsion system was composed of two R-4D LAE with a thrust of 490 N (110 lbf). It also had two axial and four radial 22 N (4.9 lbf) bipropellant thrusters for station keeping and attitude control. It included enough propellant for orbit circularization and 8 years of operation.


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