EN
Power: 260-300W;
Thrust: 30-50mN;
Specific impulse: 550s;
Ignition time: ≤2min;
Continuous working time: ≥240h;
Working lifespan: ≥400h;
Number of ignitions: ≥1000 times;
Weight: ≤0.2kg;
Thrust deflection: ≤0.5°;
Propellant: ammonia
Features:
Non-toxic and non-polluting features greatly reduce the pollution of propulsion system plumed on satellite bodies and space environment;
Low operating pressure, low system dry weight and low power consumption;
The configuration of double thrusters allows for the cold back-up of orbital control function and higher reliability;
Adopting ammonia as propellant with low storage pressure greatly reduces the complexity in testing, working range, and high-pressure risk;
Simpler system increases reliability and is superior in wight and cost;
More thrust for the same power consumption, significantly reduces mission time and greater maneuverability for unexpected situations;
Modular design of supply and thruster, simple installation interface and easy application of the system.