RD-0126
id:
rd-0126-250-5896661
title:
RD-0126
text:
The RD-0126 "Yastreb" was a liquid-fuel cryogenic rocket engine burning liquid hydrogen and liquid oxygen, developed by KBKhA Kosberg in Voronezh, Russia. The RD-0126 variant had a conventional de Laval nozzle, while the RD-0126E (РД-0126Э) was designed and constructed with an expansion-deflection nozzle. Both variants were designed to produce 39.2 kN (8,812.5 lbf) of thrust. The expansion-deflection nozzle of the RD-0126E was designed to increase the efficiency of an expander cycle by maximisin
brand slug:
wiki
category slug:
encyclopedia
description:
Russian rocket engine
original url:
https://en.wikipedia.org/wiki/RD-0126
date created:
date modified:
2023-10-03T22:15:26Z
main entity:
{"identifier":"Q118903800","url":"https://www.wikidata.org/entity/Q118903800"}
image:
fields total:
13
integrity:
14