Propulsion System Families

Four product families covering the full spectrum of spacecraft propulsion requirements — from cubesat attitude control to GEO transfer missions and deep-space applications.

4
Product Families
12+
Active Programmes
0.5–500 N
Chemical Thrust Range
3,200 s
Max EP Isp
All Families

Select a Product Family

Chemical Thrusters

0.5 N – 500 N | Mono- & Bipropellant

Hydrazine monopropellant and MMH/NTO bipropellant thruster systems for attitude control, orbit maintenance, and transfer manoeuvres.

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Electric Propulsion

Isp: 800 – 3,200 s | Hall & Ion

Hall-effect and gridded-ion thrusters for high-efficiency orbit raising, station-keeping, and deep-space missions.

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Cold Gas RCS

0.01 N – 5 N | N₂ / GN₂

Reaction control modules using inert cold gas for precision attitude manoeuvring on small satellites and cubesat platforms.

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Propellant Management

0.5 – 50 kg | Ti / SS Tanks

Integrated PMU assemblies with titanium tanks, latch valves, regulators, and structural interfaces for complete propulsion systems.

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Key Parameters

Product Family Comparison

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

Request Technical Data

Our engineering team provides mission-specific datasheets, performance maps, and qualification documentation packages. Submit an RFQ or contact us directly.