Utilizing a reliable and safe non-toxic hydroxylammonium nitrate (HAN) monopropellant propulsion system, it provides the spacecraft with the capability for rapid orbital transfer and attitude stability during orbit control. It features high thrust, green and non-toxic properties, pre-packaging capability, and fast response speed.
Thrust Magnitude | 1~5N | ||||||||||||||||||
Number of Thrusts | 1~4 | ||||||||||||||||||
Propellant Medium | Hydroxylammonium Nitrate (HAN) | ||||||||||||||||||
Pressurizing Gas | Nitrogen | ||||||||||||||||||
Maximum Continuous Thruster Duration | ≥1000s | ||||||||||||||||||
Specific Impulse | ≥210s | ||||||||||||||||||
Total Impulse | ≥4000Ns (Recommended) | ||||||||||||||||||
Dry Weight | 4kg (Standard) | ||||||||||||||||||
Power Consumption (Peak) | ≤5W (Per Thruster) |