CHEMICAL PROPULSION SYSTEM
KUMA
Bi-propellant
Bi-propellant hydrogen peroxide-kerosene propulsion systems
for small satellite platforms and nanosatellite deployers.
APPLICATIONS
KUMA Bi-propellant propulsion systems to cover small satellites multiple needs.
ORBIT RAISING
STATION KEEPING
DEORBITING
RE-POSITIONING
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.
KEROSENE
FUEL
H2O2
HTP HIGHLY STABILIZED
MAIN FEATURES
| 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 |
| Multiple restarts | Yes |
| Throttleability | 1:10 |
| 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) |
