1-20N Monopropellant System
OHB Sweden ABOHB Sweden's propulsion team has developed hydrazine-based systems for European primes, offering expertise across various thrust levels and…
123 satellite platforms, components and ground equipment from manufacturers worldwide.
OHB Sweden's propulsion team has developed hydrazine-based systems for European primes, offering expertise across various thrust levels and…
OHB Sweden AB offers a 10N Bipropellant System, supported by extensive analysis capabilities and test facilities for calibration…
Busek's Green Monopropellant Thrusters feature a patented monolithic catalyst that is efficient yet extremely robust, with available thruster…
Benchmark Space Systems offers High-Test Peroxide (HTP) propulsion systems, including the Halcyon monopropellant and Halcyon Avant bipropellant thrusters,…
The TH-31 is a space engine designed for spacecraft orbit changes and attitude control, utilizing room-temperature liquid propellants.
The TH-12 is a hundred-ton class liquid oxygen/kerosene engine designed for reusable medium and large liquid launch vehicles.
The TH-11 is an oxygen-rich staged combustion high-performance engine, using liquid oxygen/kerosene propellant, suitable for the upper stage…
DELTAV Space Technologies develops single and dual liquid-fueled propulsion systems for spacecraft maneuvering and high-performance applications, utilizing green…
HyImpulse's hybrid motor family powers suborbital and orbital vehicles with lightweight composite casings, thrust vector control, and modular…
Water-propellant resistojet for LEO in two configurations: 270 g at 3.3-4.4 mN and 250 g at 27-30 mN,…
Non-hydrazine green propellant propulsion, including modular 1U to 8U CubeSat propulsion systems offering up to 750 m/s delta-v.
Hydrazine monopropellant engine family from 0.02 lbf to 700 lbf thrust, with more than 19,000 units delivered.
556 N (125 lbf) Advanced Materials Bipropellant Rocket dual mode high performance engine for deep space and GEO…
890 N (200 lbf) dual mode high performance rocket engine for spacecraft orbit raising and maneuvering.
890 N (200 lbf) storable bipropellant rocket engine for orbit raising and in-space maneuvering.
22 N (5 lbf) storable bipropellant rocket engine for fine in-space maneuvering and attitude control.
110 N (25 lbf) storable bipropellant rocket engine for in-space maneuvering and attitude control.
490 N (110 lbf) bipropellant rocket engine from the R-4D family originally developed for the Apollo programme.
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