Delta Cryogenic Second Stage
id:
delta-cryogenic-second-stage-166-755164
title:
Delta Cryogenic Second Stage
text:
The Delta Cryogenic Second Stage (DCSS) is a family of cryogenic-fuelled rocket stages used on the Delta III, Delta IV, and on the Space Launch System Block 1 launch vehicles. The DCSS employs a unique two-tank architecture where the cylindrical liquid hydrogen (LH2) tank carries payload launch loads and forms the upper section. An oblate spheroid tank filled with liquid oxygen (LOX) and the engine are suspended from the LH2 tank and covered by the interstage during initial launch. The DCSS is p
brand slug:
wiki
category slug:
encyclopedia
description:
Japanese-American rocket stage
original url:
https://en.wikipedia.org/wiki/Delta_Cryogenic_Second_Stage
date created:
2011-01-25T21:35:44Z
date modified:
2024-08-29T19:18:07Z
main entity:
{"identifier":"Q967349","url":"https://www.wikidata.org/entity/Q967349"}
image:
{"content_url":"https://upload.wikimedia.org/wikipedia/commons/5/50/Second_stage_of_a_Delta_IV_Medium_rocket.jpg","width":3008,"height":2000}
fields total:
13
integrity:
16