Chemical Thrusters
Monopropellant and bipropellant thruster systems for attitude control, orbit maintenance, and transfer manoeuvres.
View Specifications →Chemical, electric, and cold-gas propulsion systems engineered for mission-critical reliability — from Lampoldshausen, the European centre of rocket propulsion.
From monopropellant thrusters for cubesats to bipropellant systems for GEO transfer missions — engineered to specification, not to catalogue.
Monopropellant and 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 applications.
View Specifications →Reaction control system modules using inert cold gas for precision attitude manoeuvring on small satellites and cubesat platforms.
View Specifications →Integrated propellant management units including titanium tanks, latch valves, pressure regulators, and structural interfaces.
View Specifications →ISPTech operates adjacent to the DLR Institute of Space Propulsion in Lampoldshausen — Europe's premier propulsion test infrastructure. Access to hotfire test rigs, altitude simulation chambers, and plume diagnostic instrumentation underpins every qualification programme.
Explore Test Facilities →
Optimised for mass, volume, and operational lifetime. ISPTech supports satellite bus integrators from component selection through final qualification.
Learn more →Vibration-qualified, handling-documented, and schedule-reliable. Propulsion subsystems validated to launch vehicle mechanical interface requirements.
Learn more →Full documentation trail, qualification standard compliance, and design review participation. Engineering available for programme-of-record procurement.
Learn more →ISPTech engineers present qualification results and technology developments at IAC, AIAA, and EUCASS.
Performance characterisation and environmental qualification testing of the CG-50 nitrogen cold gas thruster module, including thermal cycling, vibration, and 2,000-pulse endurance tests.
Download Paper (Registration Required) ↓Combustion stability characterisation across the operational thrust range using Rayleigh criterion analysis, pressure oscillation mapping, and injector orifice parametric study.
Download Paper (Registration Required) ↓Thrust, Isp, and efficiency measurements across the operating envelope of ISPTech's HET-200 hall thruster, with xenon propellant flow rate characterisation and plume divergence mapping.
Download Paper (Registration Required) ↓ISPTech products are designed with Wassenaar Arrangement and dual-use export regulations in mind. Our team provides export documentation support for qualified customers.
From initial requirements through qualification and delivery — our engineering team is ready. Reach out for a technical consultation or download the product catalogue.