Bipropellant Low Thrust Rocket Engine
Flight-proven UDMH/NTO bipropellant low-thrust rocket engine for spacecraft attitude control and orbit correction.
Technical specifications
- Year of release
- 1996
- Flight qualification
- Letter O1 — flight use
- Customization
- Can be adapted to customer requirements
- Propellants
- UDMH / NTO
- TRL
- 9 (flight-proven)
About
The Bipropellant Low Thrust Rocket Engine is a flight-qualified (Letter ‘O1’, flight use) UDMH/NTO bipropellant thruster designed for spacecraft propulsion systems. It was first released in 1996 and can be adapted to customer requirements. Full technical specifications are available on request through Glavkosmos.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.
