MT-2 20N Monopropellant Thruster
IHI Aerospace
Flight-proven hydrazine monopropellant thruster delivering 6.9-19.6N thrust for reaction control and station-keeping.
Technical specifications
- Thrust
- 6.9-19.6 N
- Specific Impulse
- 210-226 s
- Pulse Count
- >261,914
- Demonstrated Throughput
- >115 kg
- Status
- Flight proven
About
The MT-2 is IHI Aerospace’s 20N-class hydrazine monopropellant thruster, flight-proven with over 261,914 demonstrated pulses and used extensively for spacecraft reaction control across multiple Japanese satellite and launch vehicle programs.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.
