YF-75D
id:
yf-75d-308-2738492
title:
YF-75D
text:
The YF-75D is a liquid cryogenic rocket engine burning liquid hydrogen and liquid oxygen in a closed expander cycle. It is China's third generation of upper stage cryogenic propellant engine, after the YF-73 and the YF-75. It is used in a dual engine mount in the H5-2 second stage of the Long March 5 launch vehicles. Within the mount, each engine can gimbal individually to enable thrust vectoring control. As its predecessor, the YF-75 it can adjust its mixture ratio to optimize propellant consum
brand slug:
wiki
category slug:
encyclopedia
description:
Chinese rocket engine
original url:
https://en.wikipedia.org/wiki/YF-75D
date created:
date modified:
2023-08-05T04:46:33Z
main entity:
{"identifier":"Q21554949","url":"https://www.wikidata.org/entity/Q21554949"}
image:
fields total:
13
integrity:
14