RL60
id:
rl60-311-1156377
title:
RL60
text:
The RL60 was a planned liquid-fuel cryogenic rocket engine designed in the United States by Pratt & Whitney, burning cryogenic liquid hydrogen and liquid oxygen propellants. The engine runs on an expander cycle, running the turbopumps with waste heat absorbed from the main combustion process. This high-efficiency, waste heat based combustion cycle combined with the high-performance liquid hydrogen fuel enables the engine to reach a very high specific impulse of up to 465 seconds in a vacuum. The
brand slug:
wiki
category slug:
encyclopedia
description:
Planned US hydrolox rocket engine, intended to replace the RL10
original url:
https://en.wikipedia.org/wiki/RL60
date created:
date modified:
2023-05-06T04:42:56Z
main entity:
{"identifier":"Q3821923","url":"https://www.wikidata.org/entity/Q3821923"}
image:
fields total:
13
integrity:
14