AMBR 556 N Dual Mode High Performance Rocket Engine
Aerojet Rocketdyne (L3Harris)
556 N (125 lbf) Advanced Materials Bipropellant Rocket dual mode high performance engine for deep space and GEO missions.
Typed specifications4 values
Discloses 2 of 10 fields engineers filter by in this category (category median 3).
- Thrust
- 556 000 mN product page
- Propellant
- hydrazine product page MMH | NTO (N2O4 or MON)
Each value is typed with its unit and measurement condition and cites the datasheet page it was taken from. Nothing is guessed: a field that is absent here has not been published by the manufacturer. machine-extracted ✓ checked by NewSpace Market ✓ manufacturer confirmed by the manufacturer.
As published by the supplier3 lines, in the manufacturer's own wording
- Thrust
- 556 N (125 lbf)
- Type
- Dual mode high performance rocket engine
- Propellants
- Hydrazine or MMH fuel with NTO oxidizer
About
The AMBR is a 556 N (125 lbf) dual mode high performance rocket engine.
Bipropellant engines feed hydrazine or monomethylhydrazine (MMH) propellants and nitrogen tetroxide (NTO) oxidizer into a combustion chamber, where they ignite on contact to generate thrust. Bipropellant thrusters typically are used for in-space maneuvering for large vehicles including the crew-carrying Orion and Starliner spacecraft, as well as International Space Station servicing vehicles.
L3Harris builds monopropellant and bipropellant propulsion systems for applications including spacecraft maneuvering, orbit raising, deep space navigation, planetary landing, and rocket upper stage propulsion. These systems use storable propellants that remain stable in liquid form without the need for active cooling. In more than 60 years L3Harris has built and delivered roughly 22,000 chemical thrusters for in-space propulsion.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.