Key highlights

Green, affordable and easily available propellants: N2O + C2H6
Simple system architecture by self-pressurized system
Thrust level can be controlled by propellant temperature control
Thermal steady-state operation of the thruster allows significant deltaV from a single maneuver
Pulse mode operation allows for precise attitude control
ITAR free and REACH compliant
Cold-start capable
900 Ns impulse bit in one continuous firing demonstrated at vacuum facilities
Thruster operatable in cold gas mode as back-up option
Health-monitoring instrumentation available
Liquid fed and gasious fed

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Last updated: 2026-06-18

ISPTech