Bipropellant Low Thrust Rocket Engine
Glavkosmos
A bipropellant low-thrust rocket engine, flight-qualified and adaptable to customer requirements, released in 1996.
Technical specifications
- Year of release
- 1996
- Flight qualification of the product
- Letter "O1", flight use
- Possibility to adapt the product to customer requirements
- Yes
About
This product is a bipropellant low-thrust rocket engine, initially released in 1996. It has achieved ‘O1’ flight qualification, indicating its readiness and proven use in space applications. The manufacturer highlights the possibility of adapting the product to meet specific customer requirements, suggesting a degree of customization available for integration into various spacecraft designs. The engine’s low-thrust nature makes it suitable for precise orbital maneuvers, station-keeping, or attitude control for satellites and other spacecraft.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.