RL10
id:
rl10-168-9626955
title:
RL10
text:
The RL10 is a liquid-fuel cryogenic rocket engine built in the United States by Aerojet Rocketdyne that burns cryogenic liquid hydrogen and liquid oxygen propellants. Modern versions produce up to 110 kN (24,729 lbf) of thrust per engine in vacuum. Three RL10 versions are in production for the Centaur upper stage of the Atlas V and the DCSS of the Delta IV. Three more versions are in development for the Exploration Upper Stage of the Space Launch System and the Centaur V of the Vulcan rocket. Th
brand slug:
wiki
category slug:
encyclopedia
description:
Liquid fuel cryogenic rocket engine, typically used on rocket upper stages
original url:
https://en.wikipedia.org/wiki/RL10
date created:
2004-06-10T04:27:28Z
date modified:
2024-08-31T04:18:30Z
main entity:
{"identifier":"Q967724","url":"https://www.wikidata.org/entity/Q967724"}
image:
{"content_url":"https://upload.wikimedia.org/wikipedia/commons/6/6c/RL-10_rocket_engine_%2830432256313%29.jpg","width":3648,"height":4872}
fields total:
13
integrity:
16