
Key highlights
The system is suitable for orbital changes, orbital insertion, collision avoidance, station-keeping, and lifetime management.
It has a modular design with several elements that can be customized to mission requirements, including the tank and module size, and the thrust level.
The ARM-O uses safe, easy to handle water-based propellant and generates thrust in one direction.
The product has five variants, based on the propellant tank size; AS, A0, A1, A2, B1-B4, and is suitable for use with nano-/picosats to 6U CubeSats.
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Last updated: 2021-08-04

Technical specs
dry mass
50 g to 1500 g (depending on configuration)
wet mass
less than 50 g to 2000 g (depending on configuration)
specific impulse
100 s (estimate)
thrust
0.6 to 4 mN
power consumption
50 mW (idle)
active power
3 to 5 W/mN
command
CAN
I2C
RS485
I2C
RS485
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