MEMS Cold Gas Propulsion Module for 2-3U 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.
- Four individual thrusters with proportional thrust control
- Mass flow sensor on each thruster to provide real time thrust measurement
- Closed-loop thrust control with 20 Hz internal clock
- Integrated isolation valve as a leak tight 3rd barrier
- Integrated pressure sensors on each thruster and propellant tank
- Integrated gas heaters for improved Isp
- Integrated filter