RD-0124
id:
rd-0124-250-1526886
title:
RD-0124
text:
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 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.
brand slug:
wiki
category slug:
encyclopedia
description:
Russian rocket engine
original url:
https://en.wikipedia.org/wiki/RD-0124
date created:
date modified:
2023-05-04T05:12:19Z
main entity:
{"identifier":"Q620359","url":"https://www.wikidata.org/entity/Q620359"}
image:
{"content_url":"https://upload.wikimedia.org/wikipedia/commons/2/24/Rocket-motor-RD-0124-Salon-du-bourget-2013-DSC_0055.jpg","width":1497,"height":1586}
fields total:
13
integrity:
15