Linkedin
Linkedin

Unleash the power of in-space mobility

Our RocketPack™ can either be customized for integration into any given SmallSat platform, serve as a RCS system in a launcher, be added as a standardized external plug&play module, or be provided in an autonomous satellite bus capable of hosting the customer’s payload

Get faster everywhere

In orbit transportation

Our RocketPack is designed to solve various in-orbit-transporation missions, such as last mile deliveries and orbital transfers (LEO / LEO & GTO / GEO), and can also be used as a high-performance thruster and to optimize the payload of the launch vehicle.

Move faster everywhere

In orbit propulsion

Highlighting the versatility of our product, its missions also regroup multiple in-orbit propulsion tasks, showcasing altitude and orbit control, collision avoidance, and repositionning for the satellite using RocketPack™.

Act faster everywhere

In orbit servicing

As technologies and space servicing are improving, we are providing solutions for future missions, consisting of fast maneuver and repositionning assignments.

Ensure space sustainability

De-orbiting solution

Considering the effort of making space more and more accessible, we are willing to make it sustainable as well, by using our products as solutions to clean space debris with de-orbiting solution.

Standardized RocketPack™​

Turn-key liquid propulsion system for satellites

Rocket

MONERGOL SPECIFICATIONS

Flight Worthiness

Thruster configuration

Propellant ​

Specific Impulse

Minimum Impulse Bit

Total Impulse​

Standarized RocketPack™

monopropellant SPECIFICATIONS

Available

4 x 5 N

H202 90%

170 s​

100 mN.s​

10 - 100 kN.s

Standarized RocketPack™

monopropellant SPECIFICATIONS

Thruster configuration

4 x 5 N (Unit thrust selectable from 1 N to 20 N)​

Propellant ​

H202 (90%)

Specific Impulse

170 s​

Total Impulse​

10 kN.s / 37 kN.s / 110 kN.s

Mass (Propellant)​

6kg / 22kg / 66kg​

Mass (Dry)​

9,5kg / 14kg / 27kg

Dimensions​

0,46 m x 0.35 m / 0,46 m x 0,47 m / 0,67 m x 0,48m

Standarized RocketPack™ +

BIPROPELLANT SPECIFICATIONS

2026

4 x 20 N

H202 90% & Hydrocarbons

300 s

50 - 500 mN.s​

20 - 200 kN.s

Standarized RocketPack™ +

BIPROPELLANT SPECIFICATIONS

Thruster configuration

4 x 20 N (Unit thrust selectable from 20 N to 500 N)

Propellant ​

H202 (90%) (Ox.)
& C3H6 / Propene (Self-pressurized)(Fuel)

Specific Impulse

300 s (BiProp mode)​

Total Impulse​

30 kN.s / 75 kN.s / 220 kN.s

Mass (Propellant)​

10kg / 25kg / 75kg​

Mass (Dry)​

19kg / 24kg / 37kg​

Dimensions​

0,46 m x 0,35m / 0,46m x 0,55 m / 0,67 m x 0,58 m​

Operating temperatures

MEOP

Supply voltage

Communication

Power (Hold)

Power (Peak)

Restarts

-10°C to -50°C (14°F to -58°F)

25 bar

24-36 V

CAN / Serial RS-422

10W

50W

25 000+

Customized RocketPack™

A thrill ride on demand

Rocket

MONERGOL SPECIFICATIONS

Thruster configuration

Specific Impulse

Total Impulse​

Number of thrusters

Customized RocketPack™

monopropellant SPECIFICATIONS

4 x 5 N

170 s

5 - 150 kN.s

1 to 6

Customized RocketPack™

monopropellant SPECIFICATIONS

Thruster configuration

4 x 5 N (Unit thrust selectable from 1 N to 20 N)

Specific Impulse

170 s

Total Impulse​

5 to 150 kN.s

Number of thrusters

1 to 6

Customized RocketPack™ +

BIPROPELLANT SPECIFICATIONS

4 x 20 N

300 s

20 - 500 kN.s

1 to 6

Customized RocketPack™ +

BIPROPELLANT SPECIFICATIONS

Thruster configuration

4 x 20 N (Unit thrust selectable from 20 N to 500 N)

Specific Impulse

300 s

Total Impulse​

20 to 500 kN.s

Number of thrusters

1 to 6

Accomodate at will : Size / Layout / Thrust

Flexibility in firing mode and total impulse

Tailored reliability & redundancy

A broad field of use cases :
· Roll Attitude Control System
· Satellite propulsion
· Kick-stage
· OTV

Autonomous RocketPack™

Host customer’s payload

Autonomous RocketPack™

Up to 1200 kg LEO - GEO payload transfer

Fast GEO release < 12 hours

Storable Propellant = Responsive Launch / Launcher-agnostic

PropBall™

The tank that fuels your journey

PropBall™

Spherical membrane tank​

Compact and lightweight

Broad propellant compatibility

Long-term storability

Hypergravity and Zero-G operation​

Bolted joint accommodation​

Zero debris compliant​

Scalable in size and performance​

Affordable​

ITAR-Free