Chemical Thrusters
Hydrazine monopropellant and MMH/NTO bipropellant thruster systems for attitude control, orbit maintenance, and transfer manoeuvres.
View Specifications →Four product families covering the full spectrum of spacecraft propulsion requirements — from cubesat attitude control to GEO transfer missions and deep-space applications.
Hydrazine monopropellant and MMH/NTO bipropellant thruster systems for attitude control, orbit maintenance, and transfer manoeuvres.
View Specifications →Hall-effect and gridded-ion thrusters for high-efficiency orbit raising, station-keeping, and deep-space missions.
View Specifications →Reaction control modules using inert cold gas for precision attitude manoeuvring on small satellites and cubesat platforms.
View Specifications →Integrated PMU assemblies with titanium tanks, latch valves, regulators, and structural interfaces for complete propulsion systems.
View Specifications →High-level parameter summary across families. Contact ISPTech for mission-specific performance envelopes.
| Parameter | Chemical Thrusters | Electric Propulsion | Cold Gas RCS | Propellant Mgmt |
|---|---|---|---|---|
| Thrust Range | 0.5 – 500 N | 0.1 – 500 mN | 0.01 – 5 N | N/A (feed system) |
| Specific Impulse (Isp) | 180 – 320 s | 800 – 3,200 s | 50 – 75 s | N/A |
| Propellant | N₂H₄ / MMH+NTO | Xenon (Xe) | N₂ / GN₂ | Compatible all |
| Power (Nominal) | 20 – 120 W (valve) | 100 W – 5 kW | 8 – 25 W (valve) | 5 – 30 W |
| Min. Impulse Bit | 0.05 N·s | 0.001 N·s | 0.0002 N·s | N/A |
| Qualification Basis | ECSS-E-ST-35 / MIL | ECSS-E-ST-35 | ECSS-E-ST-35 | ECSS-E-ST-35 |
| Temperature (Operating) | -40 °C to +120 °C | -30 °C to +80 °C | -60 °C to +80 °C | -40 °C to +80 °C |
Our engineering team provides mission-specific datasheets, performance maps, and qualification documentation packages. Submit an RFQ or contact us directly.