NEMO / 2004 - on hold

Spacecraft propulsion supplied by ArianeGroup

NEMO / 2004 - on hold
	Category	Military surveillance
	Operator	US Navy
	Orbit	LEO
	Sat position	605 km x 605 km / 98°
	Launch date	Planned 2004
	Launch mass	307 kg
	Design life	7 years
	Launcher	Delta II / 7320
	Satellite / Bus	LS 400, Alenia Spazio
	Manufacturer	Space Systems / Loral

Orbital Propulsion Centre Contribution
Propulsion Responsibility: 5 x 1 N thruster (Hydrazine), CHT 1 1 x surface-tension tank, OST 31/0