HAN Non-Toxic Chemical Propulsion

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.

Description


Thrust Magnitude1~5N
Number of Thrusts1~4
Propellant MediumHydroxylammonium Nitrate (HAN)
Pressurizing GasNitrogen
Maximum Continuous Thruster Duration1000s
Specific Impulse210s
Total Impulse4000Ns (Recommended)
Dry Weight4kg (Standard)
Power Consumption (Peak)5W (Per Thruster)