Bi-propellant hydrogen peroxide-kerosene propulsion systems
for small satellite platforms and nanosatellite deployers.
KUMA Bi-propellant propulsion systems to cover small satellites multiple needs.
Our KUMA bi-propellant propulsion systems can be fully customized on thrust, expansion ratio, and accommodation to address specific customer needs and compared to currently available MMH-N2O4 units they represent a considerable trade-off between costs and performances.
HTP HIGHLY STABILIZED
|Thrust||Different systems from 1 N to 500 N (scalable to few kN)|
|Specific Impulse||> 270 s at smaller scale
> 300 s at larger scale
|Thrust time||> 100 s|
|Time to market||1.5 years (for a complete propulsion module under customer’s specs)|
|Propellant combinations||90-95% Hydrogen Peroxide – Hydrocarbons (kerosene, diesel fuel or propane)|