BT-6 22N Bipropellant Thruster
IHI Aerospace
Flight-proven 21.5N hydrazine/NTO bipropellant thruster for geostationary satellite reaction control, with 295s Isp.
Technical specifications
- Propellant
- Hydrazine / NTO
- Thrust
- 21.5 N
- Specific Impulse
- 295 s
- Inlet Pressure
- 1.69 MPa
- Demonstrated Throughput
- 583 kg
- Status
- Flight proven
About
The BT-6 is IHI Aerospace’s 22N-class bipropellant thruster using hydrazine and NTO propellants, developed alongside the BT-4 450N thruster for geostationary satellite propulsion systems. It is flight-proven with a demonstrated propellant throughput of 583 kg.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.
