COSHGT high-performance green thruster uses non-toxic, high-energy liquid Hydroxylammonium nitrate (HAN) as a propellant, which has been successfully applied in orbit in China. The structure includes a propellant tank, a front-end solenoid valve, a thruster assembly (including starting solenoid valve), a pressure sensor, a gas charging and exhaust valve, a liquid adding and exhaust valve and other modules with the blowdown design, the rated output thrust of the thruster is 0.5N. The total impulse can be up to 1100N.s, which could be used for the attitude and orbit control in steady-state & pulse mode. The system is prepackaged and does not need on-site refueling.

The full angle of the plume: 30°;

Cumulative number of pulses: 10000;

Size: 96mm×91.19mm×149.18mm;

Mass: ≤1300g;