Samiksha Jaiswal (Editor)

HS 376

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Country of origin
  
United States

Power
  
800 to 2,000 Watts

Built
  
58

Derivative
  
HS-393

Spacecraft type
  
Spin-stabilized

Status
  
Retired

Launch date
  
12 April 1985

Derived from
  
HS-333

Applications
  
Communications satellite

Manufacturer
  
Boeing Satellite Development Center

Similar
  
Spacebus, IndoStar‑1, Telkom‑2, Morelos Satellite, Paksat‑1

The Boeing 376 (sometimes referred to as the BSS-376, and previously as the HS-376) is a communications satellite bus introduced in 1978 by Hughes Space and Communications Company. It was a spin-stabilized bus that the manufacturer claims was the first standardized platform.

Contents

Design

The satellite bus was designed and manufactured by Hughes. This spin-stabilized platform had two main sections. One, the spinning section, was kept rotating at 50 rpm to maintain attitude, and a despun section that was used by the payload to maintain radio coverage.

The spinning section included the Apogee kick motor, most of the attitude control, the power subsystem and the command and telemetry subsystems. The despun section contained the communications payload, including the antennas and transponders.

The stock version had a launch mass of 1,100 to 1,450 kg (2,430 to 3,200 lb), a mass of 540 to 790 kg (1,190 to 1,740 lb) after reaching geostationary orbit and an 8 to 10-year design life. When stowed for launch, its dimensions were 2.8 to 3.15 m (9 ft 2 in to 10 ft 4 in) in height and 2.16 m (7 ft 1 in) in diameter. With its solar panels fully extended its height was 6.6 to 8 m (22 to 26 ft).

Its power system generated approximately 1,100 Watts to 1,200 Watts of power at BOL, thanks to two cylindrical solar panels.The bottom panel was retracted around the body and top panel for launch, and extended downwards for operation. It also had a two NiCd batteries for solar eclipses.

Versions

There were four variations of this platform:

  • HS-376: The original version of the platform was launched in 1977. It had a mass between 1.1 to 1.45 t (1.21 to 1.60 tons).
  • HS-376L: The Longer life version of the platform was launched in 1991. It had reduced power of 700 Watts and reduced electronics weight, which allowed for increased station keeping propellant supply. This lengthened the design life to 13.5 years.
  • HS-376HP: A Higher Power version of the platform was launched in 1995. It had a mass between 1.45 to 1.55 t (1.60 to 1.71 tons).
  • HS-376W: The Wide version of the platform was launched in 1990. It was wider, more powerful and modernized electronics. It was a joint development with INPE. It had a diameter of 3.43 m (11.3 ft) and more power.

    • Satellites

    The HS-376 was a very successful satellite platform with 58 satellites ordered, built and launched. It was also the first satellite to launch from the Space Shuttle.

    References

    HS-376 Wikipedia
    (Text) CC BY-SA