Pleiades 1A

Spacecraft propulsion supplied by ArianeGroup

Pleiades 1A
	Category	Earth Observation
	Operator	CNES
	Orbit	LEO
	Sat position	695 x 695 km
	Launch date	17.12.2011
	Launch mass	970 kg
	Design life	5 years
	Launcher	Soyuz STA Fregat
	Satellite / Bus	AstroSat 1000
	Manufacturer	EADS Astrium (prime), Alcatel

Orbital Propulsion Centre Contribution
Propulsion Responsibility: Complete system, incl: 4 x 1 N hydrazine thrusters Propellant Tank OST 31/0 Latch valve 3 x Fill and drain valves