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Cluster II - FM5, -FM6, -FM7, -FM8 / 2000-041A, 041B, 045A, 045B

Spacecraft propulsion supplied by ArianeGroup

Cluster II - FM5, -FM6, -FM7, -FM8 / 2000-041A, 041B, 045A, 045B
European Space AgencyCluster Category Science
Operator ESA
Orbit High elliptical
Sat position 17,200 km x 125,000 km
Launch date 16.7.2000
Launch mass 1200 kg
Design life 4 years
Launcher Soyuz-Fregat
Satellite / Bus -
Manufacturer Astrium GmbH


Orbital Propulsion Centre Contribution
Propulsion Contribution:
bullet 1 x 400 N N2O4 / MMH thruster, S400-10
bullet 8 x 10 N N2O4 / MMH thruster, S10-13
400 N thruster S400-10
10 N bipropellant thruster S10-13


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