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MEMS Cold Gas Propulsion Module for 6U+ nanosatellites 

The MEMS-propulsion module contains four individually controllable thrusters with integrated flow sensors to provide real time thrust measurements. 

Thrust range can be tailored to specific needs in the micro- to milli-Newton range.

Main features

  • Four individual thrusters with proportional thrust control
  • 2 separate main tanks with Butane
  • Mass flow sensor on each thruster to provide real time thrust measurement
  • Closed-loop thrust control
  • Integrated isolation valve as a leak tight 3rd barrier 
  • Integrated pressure sensors on each thruster and propellant tank
  • Integrated gas heaters for improved Isp
  • Compatible with GomSpace 6U structure
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