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RD-0124 (14D23)

Chemical Automatics Design Bureau · liquid · Russia · Modern (1992–2009)

RD-0124 (14D23) — liquid
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The RD-0124 is a rocket engine burning liquid oxygen and kerosene in an oxygen-rich staged combustion cycle, developed by the Chemical Automatics Design Bureau in Voronezh. RD-0124 engines are used on the Block I stage used on Soyuz-2.1b and Soyuz-2.1v. A variant of the engine, the RD-0124A, is used on the Angara rocket family's URM-2 upper stage.

Specifications

Category
Fixed Wing
Sub-Category
UAV
Domain
Defence
Era
Modern (1992–2009)
Country
Russia
Manufacturer
Chemical Automatics Design Bureau
Primary Role
liquid
Status
In production