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RD-843

Ukrainian single nozzle liquid propellant rocket engine From Wikipedia, the free encyclopedia

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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]

Quick facts Country of origin, First flight ...

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]

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See also

  • AVUM - The upper stage of the Vega rocket that uses the RD-843 as its main engine.
  • Vega - The ESA small rocket that uses AVUM.
  • Yuzhnoe Design Bureau - The RD-843 designer bureau.
  • Yuzhmash - A multi-product machine-building company that's closely related to Yuzhnoe and manufactures the RD-843.

Notes

  1. Engine can burn up to 612.5 seconds per burn. Maximum cumulative burn time of 924.8 seconds.

References

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