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Spacecraft design
 
The Rosetta Orbiter - Spacecraft design
 
 
Spacecraft design
 
Rosetta resembles a large aluminium box whose dimensions are 2.8 x 2.1 x 2.0 metres. The scientific instruments are mounted on the 'top' of the box – the Payload Support Module – while the subsystems are on the 'base' or Bus Support Module.
 
On one side of the Orbiter is a 2.2 metre-diameter communications dish – the steerable high-gain antenna – while the Lander is attached to the opposite face. Two enormous solar wings extend from the other sides. These panels, each 32 square metres in area, have a total span of about 32 m tip-to-tip. Each of them comprises five panels, and both may be rotated through ±180 degrees to catch the maximum amount of sunlight.

In the vicinity of Comet Wirtanen, the scientific instruments will almost always point towards the comet, while the antennas and solar arrays point towards the Sun and Earth (at large distances, they are looking more or less in the same direction).

In contrast, the Orbiter's side and back panels are in shade for most of the mission. Since these panels receive little sunlight, they are an ideal location for the spacecraft's radiators and louvers. They will also face away from the comet, so damage from comet dust will be minimised.
 
 
Propulsion
 
At the heart of the Orbiter is the main propulsion system. Mounted around a vertical thrust tube are two large propellant tanks, the upper one containing fuel, and the lower one containing the oxidiser. The Orbiter also carries 24 thrusters for trajectory and attitude control. Each of these thrusters pushes the spacecraft with a force of 10 Newton, equivalent to that experienced by someone holding a bag of 10 apples. Over half the launch weight of the entire spacecraft is taken up by propellant.
 
 
Spacecraft Vital Statistics 
Size 
  main structure2.8 x 2.1 x 2.0 metres
  diameter of solar arrays32 metres
Launch mass 
  total3,000 kg (approx.)
  propellant1,670 kg (approx.)
  science payload165 kg
  lander100 kg
Solar array output850 W at 3.4 AU, 395 W at 5.25 AU
Propulsion subsystem24 bi-propellant 10N thrusters
Operational mission10,5 years
 
 

Last update: 12 December 2002
 
 
 
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