LE-5
id:
le-5-241-4798075
title:
LE-5
text:
The LE-5 liquid rocket engine and its derivative models were developed in Japan to meet the need for an upper stage propulsion system for the H-I and H-II series of launch vehicles. It is a bipropellant design, using LH2 and LOX. Primary design and production work was carried out by Mitsubishi Heavy Industries. In terms of liquid rockets, it is a fairly small engine, both in size and thrust output, being in the 89 kN (20,000 lbf) and the more recent models the 130 kN (30,000 lbf) thrust class. T
brand slug:
wiki
category slug:
encyclopedia
description:
Japanese hydrolox rocket engine used on the H3 upper stage
original url:
https://en.wikipedia.org/wiki/LE-5
date created:
date modified:
2024-03-22T05:06:55Z
main entity:
{"identifier":"Q1054827","url":"https://www.wikidata.org/entity/Q1054827"}
image:
{"content_url":"https://upload.wikimedia.org/wikipedia/commons/4/4e/LE-5.JPG","width":810,"height":1440}
fields total:
13
integrity:
15