Eureca / 1992 - 049B

Spacecraft propulsion supplied by ArianeGroup

Eureca / 1992 - 049B
	Category	Science
	Operator	ESA
	Orbit	LEO
	Sat position	438 km
	Launch date	31.7.1992
	Launch mass	4450 kg
	Design life	11 months
	Launcher	Atlantis
	Satellite / Bus	-
	Manufacturer	Deutsche Aerospace (DASA)

Orbital Propulsion Centre Contribution
Propulsion responsibility: 8 x 20 N hydrazine thrusters, CHT 20 12 x 20 mN N2 cold gas thrusters, CGT 1 1 x 15 mN ion thruster, RITA Fill & Drain valves Latch valve LP