Rahul Sharma (Editor)

RD 193

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Country of origin
  
Russia

Designer
  
Predecessor
  
Date
  
2011

Application
  
Main engine

Propellant
  
LOX / RP-1

RD-193

The RD-193 is a high performance single-combustion chamber rocket engine, developed in Russia from 2011 to 2013. It is derived from the RD-170 originally used in the Energia launcher.

The RD-193 is fueled by a kerosene / LOX mixture and uses an oxygen-rich staged combustion cycle. RD-193 was proposed as a replacement for the NK-33, which is being used in the Soyuz-2-1v vehicle.

Design

The engine is a simplified version of the RD-191. Characterized by the absence of swing assembly chamber and related to other structural elements, thus reducing the size and weight (300 kg) and lower its cost.

References

RD-193 Wikipedia


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