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Slide Show
Slide 71

 

ISO / 1995 - 062A

Spacecraft propulsion supplied by ArianeGroup

ISO / 1995 - 062A
ESA
ISO Spacecraft
Category Science
Operator ESA
Orbit High elliptical
Sat position 1038 km x 70569 km
Launch date 1995
Launch mass 2498 kg
Design life 2 years
Launcher Ariane 44P
Satellite / Bus -
Manufacturer ESA

 

Orbital Propulsion Centre Contribution
Subsystem responsibility:
bullet 8 x 2 N hydrazine thruster, CHT 2
bullet Fill & Drain valves
2N hydrazine thrusterFill and drain valves

 

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