CHEMICAL MOTORS

Bi-propellant

Bi-propellant hydrogen peroxide-kerosene propulsion systems
for small satellite platforms and nanosatellite deployers.

APPLICATIONS

Bi-propellant propulsion systems to cover small satellites multiple needs.

ORBIT RAISING

STATION KEEPING

DEORBITING

RE-POSITIONING

Our 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

5

TRL

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)