M010 Micro-Thruster
Micro Aerospace Solutions
Miniature cold-gas micro-thruster: 0.05N thrust, 160s Isp, 12g, 0.5W, Tridyne non-toxic propellant, <100,000 pulses, for CubeSat and nanosatellite propulsion.
Technical specifications
- Thrust
- 0.05 N
- Specific Impulse
- 160 s
- Propellant
- Tridyne cold gas (N2/H2/O2)
- Mass
- 12 g
- Power
- 0.5 W
- Inlet Pressure
- 350,000 Pa
- Max Pulses
- <100,000
About
The Micro Aerospace Solutions M010 is a miniature cold-gas micro-thruster using Tridyne propellant for CubeSat and nanosatellite propulsion. Delivering 0.05 N thrust with 160 s specific impulse, the M010 is 10x more thrust than the M005 at 12g mass and 0.5W power. Non-toxic propellant enables safe secondary payload integration.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.
