MT-2 Monopropellant Thruster
IHI Aerospace flight-proven 20N-class hydrazine monopropellant thruster with 6.9–19.6N thrust, >261,914 demonstrated pulses and >115 kg throughput.
Technical specifications
- Propellant
- Hydrazine
- Thrust Range
- 6.9–19.6 N
- Specific Impulse
- 210–226 s
- Demonstrated Pulses
- >261,914
- Propellant Throughput
- >115 kg
- Heritage
- Flight proven
About
The IHI Aerospace MT-2 is a 20N-class flight-proven hydrazine monopropellant thruster. Delivering 6.9–19.6 N thrust with 210–226 s specific impulse, the MT-2 has accumulated over 261,914 demonstrated pulse firings and greater than 115 kg propellant throughput. Used for delta-V and attitude control on a wide range of Japanese and international spacecraft.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.