BT-6 Bipropellant Thruster
IHI Aerospace
IHI Aerospace flight-proven 22N bipropellant thruster using Hydrazine/NTO with 295s Isp and 583 kg demonstrated propellant throughput.
Technical specifications
- Propellant
- Hydrazine / NTO (bipropellant)
- Thrust
- 21.5 N
- Specific Impulse
- 295 s
- Inlet Pressure
- 1.69 MPa
- Propellant Throughput
- 583 kg
- Heritage
- Flight proven
About
The IHI Aerospace BT-6 is a 21.5 N flight-proven bipropellant thruster using Hydrazine/NTO propellants. With 295 s specific impulse, 1.69 MPa inlet pressure, and 583 kg demonstrated propellant throughput, the BT-6 provides precise attitude and orbit control for geostationary and deep space missions requiring bipropellant efficiency at moderate thrust levels.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.
