HBT-1 Bipropellant Thruster
IHI Aerospace
IHI Aerospace flight-proven 124N bipropellant thruster using MMH/MON3 with 274.9s Isp, 40,000s demonstrated life and 446 kg throughput.
Technical specifications
- Propellant
- MMH / MON3 (bipropellant)
- Thrust
- 124.4 N
- Specific Impulse
- 274.9 s
- Inlet Pressure
- 2.05 MPa
- Demonstrated Life
- 40,000 s
- Propellant Throughput
- 446 kg
- Heritage
- Flight proven
About
The IHI Aerospace HBT-1 is a 124.4 N flight-proven bipropellant thruster using MMH/MON3 propellants. With 274.9 s specific impulse, 2.05 MPa inlet pressure, 40,000 s demonstrated life, and 446 kg propellant throughput, the HBT-1 provides high-efficiency orbit insertion and attitude control for medium and large satellites.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.
