CHEMICAL MOTORS
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 12:1 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.
