HYBRID PROPULSION TECHNOLOGY FOR SMALL LAUNCH VEHICLES
Hybrid Propulsion
Hybrid rocket propulsion combines fuel dense solid grain and a liquid oxidizer, taking advantage of both the fuel density of the solid fuel and the simplicity of the integrated engine system. Hybrid engines are throttlable and can be shut down and restarted during flight making the technology ideal for use in upper stage modules
Our Technolgy
Modular
Lightweight
The engine design can be clustered together to lift larger modules, enabling the vehicles total propulsive power to be optimalized for different needs
The high thrust to weight ratio of the solid fuel grain and the lightweight system involved in hybrid propulsion makes the engine ideal for small satellite launch vehicles
Solid fuel grain produced using additive manufacturing have the ability to give the engine a steadier regression rate. This increases the expected energetic combustion of the fuel grain and provides a smoother engine burn
