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Slide 160

 

COSMO - SkyMed 2 / 2005

Spacecraft propulsion supplied by ArianeGroup

COSMO - SkyMed 2 / 2005
Italian Space AgencyCosmo SkyMed Category Remote Sensing
Operator ASI
Orbit  
Sat position 620 km x 620 km
Launch date 09.12.2007
Launch mass 1900 kg
Design life 5 years
Launcher Delta 7420-10C
Satellite / Bus Primabus
Manufacturer Alenia Spazio SpA

 

Orbital Propulsion Centre Contribution
Propulsion Responsibility:
bullet 6 x 1 N thruster (Hydrazine), CHT 1
bullet 1 x surface-tension tank, OST 31/0
bullet 2 x Fill & drain valves


Hydrazine propellant tank
1 N hydrazine thruster

 

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