RD-263
id:
rd-263-291-17843193
title:
RD-263
text:
The RD-263 is a liquid rocket engine, burning N2O4 and UDMH in the oxidizer rich staged combustion cycle. Four RD-263 engines form a propulsion module RD-264. For the R-36M KB Yuzhnoye only ordered the first stage propulsion to Energomash, instead of both stages, arguing that they were overworked with the RD-270 development. By April 1970 Yuzhnoye was getting the engine documentation. By the end of 1972 Energomash started to test fire the engines in its own test stand. And by September 1973 the
brand slug:
wiki
category slug:
encyclopedia
description:
Rocket engine
original url:
https://en.wikipedia.org/wiki/RD-263
date created:
date modified:
2023-10-04T19:13:27Z
main entity:
{"identifier":"Q20203126","url":"https://www.wikidata.org/entity/Q20203126"}
image:
fields total:
13
integrity:
14