Loading AI tools
Ukrainian single nozzle liquid propellant rocket engine From Wikipedia, the free encyclopedia
The RD-843 is a Ukrainian single nozzle liquid propellant rocket engine. It burns a hypergolic mixture of unsymmetrical dimethylhydrazine (UDMH) fuel with dinitrogen tetroxide (N2O4) oxidizer. It is pressure-fed. It is rated for up to 5 restarts, and can gimbal up to 10 degrees in each direction.[2]
Country of origin | Ukraine |
---|---|
First flight | 2012-02-13 |
Designer | Yuzhnoye Design Bureau |
Manufacturer | Yuzhmash |
Application | Upper stage |
Associated LV | Vega, Vega C |
Predecessor | RD-869 |
Status | In production |
Liquid-fuel engine | |
Propellant | N2O4 / UDMH |
Mixture ratio | 2.0 |
Cycle | Pressure-fed |
Configuration | |
Chamber | 1 |
Performance | |
Thrust, vacuum | 2.452 kN (551 lbf) |
Chamber pressure | 2.04 MPa (296 psi) |
Specific impulse, vacuum |
|
Burn time |
|
Restarts | Up to 5 |
Gimbal range | ±10° |
Dimensions | |
Dry mass | 15.93 kg (35.1 lb) |
Used in | |
AVUM, AVUM+ | |
References | |
References | [1][2][3][4] |
It was developed by Yuzhnoye Design Bureau for Avio and is manufactured by Yuzhmash. It uses the RD-869 thrust chamber, the old Soviet ICBM SS-18 final stage engine from which it is evolved, and which was also designed by Yuzhnoye. The RD-843 ground test campaign included 74 tests, 140 ignitions, reaching a total of 8,201 seconds, which is approximately 12 service lives on 4 engines. As of June 2020 it has been successfully used on 14 orbital launches.[5]
The Vega and Vega C uses it as the main engine on its AVUM (Attitude & Vernier Upper Module) fourth stage which it calls the MEA (short for Main Engine AVUM).[6]
Seamless Wikipedia browsing. On steroids.
Every time you click a link to Wikipedia, Wiktionary or Wikiquote in your browser's search results, it will show the modern Wikiwand interface.
Wikiwand extension is a five stars, simple, with minimum permission required to keep your browsing private, safe and transparent.