M100 Micro-Thruster
1N hydrogen peroxide monopropellant micro-thruster: 200s Isp, 30g, 2W, unique metal gauze catalyst, <100,000 pulses, for small satellite delta-V and attitude control.
Technical specifications
- Thrust
- 1.0 N
- Specific Impulse
- 200 s
- Propellant
- Hydrogen peroxide (H2O2), green monopropellant
- Catalyst
- Metal gauze catalyst
- Mass
- 30 g
- Power
- 2.0 W
- Inlet Pressure
- 350,000 Pa
- Max Pulses
- <100,000
About
The Micro Aerospace Solutions M100 is a 1 N hydrogen peroxide monopropellant micro-thruster with a unique metal gauze catalyst for reliable propellant decomposition. Delivering 1.0 N thrust with 200 s specific impulse, the M100 provides significant delta-V capability for small satellites at 30g mass and 2.0W power. The 200s Isp is notably high for H2O2 monopropellant thrusters at this size, enabling efficient orbit maintenance and attitude control.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.