Shaping the future of in-space mobility

Our Rocket Pack 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 Rocket Pack 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 sattelite using Rocket Pack .

“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”

Deorbitation service

Considering the effort of making space more and more accesible, we are willing to make it sustainable as well, by using our products as solutions to clean space debris with deorbitaion services.

STANDARDIZED ROCKETPACK™

“Turn-key liquid propulsion system for satellites”

Rocket

MONERGOL SPECIFICATIONS

Thruster configuration

Propellant ​

Specific Impulse

Total Impulse​

Mass (Propellant)​

Mass (Dry)​

Dimensions​

Rocketpack standard™

monopropellant SPECIFICATIONS

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

H202 (90%)

170 s​

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

6kg / 22kg / 66kg​

9,5kg / 14kg / 27kg

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

Rocketpack standard™ +

BIPROPELLANT SPECIFICATIONS

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

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

300 s (BiProp mode)​

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

10kg / 25kg / 75kg​

19kg / 24kg / 37kg​

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

Operating temperatures

Tank pressure

Supply voltage

Communication

Power (Hold)

Power (Peak)

Restarts

-10°C to -50°C (14°F to -58°F)

<30 bar

24-36 V

CAN / Serial RS-422

10W

50W (4 thrusters together)

25 000+

CUSTOMIZED ROCKETPACK™

“A thrill ride on demand”

Rocket

MONERGOL SPECIFICATIONS

Thruster configuration

Specific Impulse

Total Impulse​

Number of thrusters

Customized standard™

monopropellant SPECIFICATIONS

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

170 s

5 to 150 kN.s

1 to 6

Customized standard™ +

BIPROPELLANT SPECIFICATIONS

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

300 s

20 to 500 kN.s

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™

1500 kg LEO - GEO payload transfer

Fast GEO release < 12 hours

Storable propellants = responsive launch

Launcher-agnostic
· Falcon 9
· Ariane 6
· VEGA-C/E
· ISAR
· MAIA