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Slide 230

 

Theos (Thaichote)

Spacecraft propulsion supplied by ArianeGroup

Theos (Thaichote)
Gistda logo.theos. Category Earth Observation
Operator GISTDA
Orbit LEO
Sat position 820km
Launch date 01.10.2008
Launch mass 750 kg
Design life -
Launcher Dnepr
Satellite / Bus Leostar 500 XO
Manufacturer EADS Astrium

 

Orbital Propulsion Centre Contribution
Propulsion Responsibility:
Complete system, incl:
bullet 4 x 1 N hydrazine thrusters
bullet Propellant tank OST 33/0 
bullet Fill & drain valves   
1 N hydrazine thruster. propellant tank.

Fill and drain valve.

 

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