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RD 801

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Country of origin
  
Ukraine

Manufacturer
  
Yuzhmash

Status
  
In development

Designer
  
Yuzhnoye Design Bureau

Application
  
First Stage

Propellant
  
LOX / RG-1

RD-801

The RD-801 (Russian: РД-801) is an Ukrainian liquid propellant rocket engine burning LOX and Kerosene (RG-1) in a staged combustion cycle. It has a single combustion chambers that provide thrust vector control by gimbaling of the nozzle in two axis by +/- 6°. It is being designed in Ukraine by Yuzhnoye Design Bureau for the prospective first stage propulsion of the Mayak rocket family.

The RD-801 as well as the RD-810 are being designed based on the work of the RD-8 vernier and the maintenance and improvement of the RD-120 engines. The RD-801 can be used stand alone on a Mayak or in a cluster.

Versions

The designers have proposed three versions of this engine:

  • RD-801 (version 0) (Russian: РД-801 (исполнение 0)): This is the basic module with no TVC.
  • RD-801 (version 01) (Russian: РД-801 (исполнение 01)): This is a version which includes a TVC by gimbaling of the nozzle in two axis by +/- 6°.
  • RD-801V (Russian: РД-801В): High altitude of the rocket engine with extended nozzle.

    • References

    RD-801 Wikipedia
    (Text) CC BY-SA


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