Giotto / 1985 - 056A

Spacecraft propulsion supplied by ArianeGroup

Giotto / 1985 - 056A
	Category	Science
	Operator	ESA
	Orbit	Heliocentric
	Sat position	-
	Launch date	2.7.1985
	Launch mass	960 kg
	Design life	1 year (achieved: 6 years)
	Launcher	Ariane 1
	Satellite / Bus
	Manufacturer	Dornier

Orbital Propulsion Centre Contribution
Subsystem responsibility: 8 x 20 N hydrazine thruster, CHT 2 with 90° canted nozzle Fill & Drain valves Propellant loading in Kourou