RD-0110R
id:
rd-0110r-247-18425878
title:
RD-0110R
text:
The RD-0110R is a rocket engine burning kerosene in liquid oxygen in a gas generator combustion cycle. It has four nozzles that can gimbal up to 45 degrees in a single axis and is used as the vernier thruster on the Soyuz-2-1v first stage. It also has heat exchangers that heat oxygen and helium to pressurize the LOX and RG-1 tanks of the Soyuz-2.1v first stage, respectively. The oxygen is supplied from the same LOX tank in liquid form, while the helium is supplied from separate high pressure bot
brand slug:
wiki
category slug:
encyclopedia
description:
original url:
https://en.wikipedia.org/wiki/RD-0110R
date created:
date modified:
2023-07-24T01:59:07Z
main entity:
{"identifier":"Q12146473","url":"https://www.wikidata.org/entity/Q12146473"}
image:
{"content_url":"https://upload.wikimedia.org/wikipedia/commons/7/72/PlesetskRocketLaunch2019-02.jpg","width":1200,"height":800}
fields total:
13
integrity:
14