R-42DM 890 N Dual Mode High Performance Rocket Engine
Aerojet Rocketdyne (L3Harris)
890 N (200 lbf) dual mode high performance rocket engine for spacecraft orbit raising and maneuvering.
Key figurescomparable across the catalogue
- Thrust
- 890 N
Normalised to common units so this product can be compared with others in its category. The supplier's own wording is below.
As published by the supplier
- Thrust
- 890 N (200 lbf)
- Type
- Dual mode high performance rocket engine
- Propellants
- Hydrazine or MMH fuel with NTO oxidizer
About
The R-42DM is an 890 N (200 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.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.