123 satellite platforms, components and ground equipment from manufacturers worldwide.
The Rafael 25N Monopropellant Hydrazine Thruster is designed for high-thrust satellite maneuvers, providing 9.5 to 28 N of…
The Rafael 5N Monopropellant Hydrazine Thruster is designed for satellite attitude control and orbit correction maneuvers. It produces…
The Rafael 1N Monopropellant Hydrazine Thruster generates the required thrust for maneuvering satellites by means of a hot…
HAN-based liquid monopropellant family, electrically ignitable or catalyst-bed ignitable, in GEM3 and Sierra GEM variants.
HAN-based green liquid monopropellant, higher performance and lower toxicity than hydrazine, used in NASA GPIM.
The E-2 is a LOX/Kerosene oxidizer-rich staged combustion engine designed for small launch vehicles, aiming to be the…
Advanced green hypergolic H2O2 + ionic liquid multi-mode propulsion, up to 310 s Isp, 20-200 N.
High-precision chemical thruster with closed-loop pressure control, 20-200 N thrust range.
Family of High Test Peroxide (HTP) monopropellant thrusters (ALPHARD-10, -10-HP, -20, -20-HP, -200) for delta-v and RCS on…
ATOM is a next-generation monopropellant thruster designed for CubeSats, offering high-performance thrust starting from 1N using an eco-friendly,…
Thrust Vector Control systems for solid and hybrid motor launch vehicles using flex nozzle, engine gimbaling, or liquid…
Miniaturized propulsion combining main thruster with 3-axis attitude control — non-toxic self-pressurizing propellants, 120M+ valve actuations, 0.54U CHIPS-180…
High-thrust monopropellant propulsion using proprietary CMP-X ethanol/hydrogen-peroxide blend — safer, lower-cost alternative to hydrazine, >2,000 Ns total impulse.
Next-generation monopropellant thruster using eco-friendly, nontoxic propellant — starting from 1N thrust, for 1U to 26U+ CubeSats, 30x…
Modular hybrid propulsion unit using solid HDPE fuel and N2O oxidizer for last-mile orbital maneuvers of small satellites…
Mission-configured, high-thrust green chemical propulsion system for satellites, enabling fast orbit transfer, collision avoidance, in-orbit servicing, and re-entry…
GP-LAM is a compact, modular, and safe 300 N green thruster designed for upper stages of Launch Vehicles,…
Green chemical propulsion system with 4x1N thrusters for 100-500kg satellites — hydrazine-free alternative delivered to India's DRDO for…
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