CHEMICAL THRUSTERS

Hybrid Propellant


Simple, Versatile and Cost Effective
Hybrid Rocket propulsion systems
our product

Hybrid
Propellant

Simple, Versatile and Cost Effective Hybrid Rocket propulsion systems to provide mobility to satellite platforms and large deployers in a range between 100 N to 10 kN of thrust.

KEY FEATURES
BENEFITS

Low cost

The system is specifically conceived to represent a trade off between costs and performances, targeting a substantial cost reduction respect to currently available, MMH-N2O4 bi-propellant units.

Customizable

The system is customizable on thrust, expansion ratio and accommodation to fit specific customer needs.

Green

Hydrogen peroxide is a green non toxic oxidizer. Furthermore our system uses highly stabilized peroxide which, respect to MIL-Grade peroxide allows for reduced compatibility issues. Different type of solid fuels can be used depending on customer needs, all of them are not reactive and not toxic.

Restartable

The system is restartable many times.

Throttleable

The system allows for a 1:5 throttleability.

Performance

Current delivered specific impulse 285 s.

APPLICATIONS

Orbit raising, Orbit changes, Decommissioning, KO motor.

ACHIEVEMENTS

Different versions of the motor are under development since 2014. Several laboratory models have been developed and tested. A 500 N Engineering model is under development. Currently TRL 5/6.

DEVELOPMENT

Developments are currently ongoing to target TRL 6.