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
	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: 1 x 400 N N2O4 / MMH thruster, S400-10 8 x 10 N N2O4 / MMH thruster, S10-13