About: Delta Cryogenic Second Stage

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The Delta Cryogenic Second Stage (DCSS) is a family of cryogenic rocket stages used on the Delta III and Delta IV rockets, and on the Space Launch System Block 1. The stage consists of a cylindrical liquid hydrogen (LH2) tank structurally separated from an oblate spheroid liquid oxygen (LOX) tank. The LH2 tank cylinder carries payload launch loads, while the LOX tank and engine are suspended below within the rocket's inter-stage. The stage is powered by a single Aerojet Rocketdyne-Pratt & Whitney RL10B-2 engine, which features an extendable carbon-carbon nozzle to improve specific impulse.

Attributes	Values
rdf:type	yago:Abstraction100002137 yago:FundamentalQuantity113575869 yago:Measure100033615 yago:Phase115290337 yago:TimePeriod115113229
rdfs:label	Delta Cryogenic Second Stage (en) Delta Cryogenic Second Stage (in) Delta Cryogenic Second Stage (fr) Delta Cryogenic Second Stage (it) Delta Cryogenic Second Stage (pl) Delta Cryogenic Second Stage (pt)
rdfs:comment	The Delta Cryogenic Second Stage (DCSS) is a family of cryogenic rocket stages used on the Delta III and Delta IV rockets, and on the Space Launch System Block 1. The stage consists of a cylindrical liquid hydrogen (LH2) tank structurally separated from an oblate spheroid liquid oxygen (LOX) tank. The LH2 tank cylinder carries payload launch loads, while the LOX tank and engine are suspended below within the rocket's inter-stage. The stage is powered by a single Aerojet Rocketdyne-Pratt & Whitney RL10B-2 engine, which features an extendable carbon-carbon nozzle to improve specific impulse. (en) Le Delta Cryogenic Second Stage (DCSS) est une famille d'étages supérieurs de fusée utilisée sur les lanceurs Delta III et Delta IV, et prévue d'être utilisée sur le lanceur lourd Space Launch System. (fr) Delta Cryogenic Second Stage (DCSS) adalah keluarga dari tahapan roket cryogenic digunakan pada roket delta III & Delta IV, dan yang rencananya akan digunakan pada Block I Space Launch System. Tahapan ini didukung oleh satu mesin Pratt & Whitney RL10B-2, yang memiliki nozzle karbon-karbon diperpanjang untuk meningkatkan dorongan tertentu. (in) Il Delta Cryogenic Second Stage (DCSS) è una famiglia di stadi a razzo criogenici usata sui veicoli di lancio Delta III e Delta IV e il cui utilizzo è previsto anche a bordo del Block 1 dello Space Launch System. Lo stadio consiste in un serbatoio cilindrico dell'idrogeno liquido strutturalmente separato da un serbatoio sferico dell'ossigeno liquido. Il cilindro del LH2 trasporta i carichi utili in ogni lancio, mentre il motore e il serbatoio LOX sono sospesi nell'interstadio del razzo. Lo stadio è alimentato da un singolo motore Pratt & Whitney RL10-B-2 fornito di un ugello al carbonio espandibile fornendo un elevato impulso specifico. (it) Delta Cryogenic Second Stage (DCSS) – stopień górny rakiet nośnych Delta III i Delta IV. Jako jednostkę napędową wykorzystuje silnik , używany w członach i Centaur, z poważnymi modyfikacjami (większa moc, rozszerzalna komora spalania, wychylanie elektromechaniczne). W przyszłości ma być użyty z rakietami Space Launch System (pod nazwą Interim Cryogenic Propulsion Stage). (pl) O Delta Cryogenic Second Stage (DCSS), é um estágio de foguete, movido a combustíveis líquidos criogênicos, no caso, LH2 e LOX, usado no foguete Delta IV, como parte de um sistema de foguete modular. O DCSS, é usado nos foguetes Delta III e Delta IV, e também está planejado que seja usado no futuro Space Launch System. O Delta Cryogenic Second Stage, tem três variantes: duas com 4 m de diâmetro, sendo uma com 8,8 m de altura e outra com 12,2 m, a terceira, tem 5 m de diâmetro e 13,7 m de altura. Todas essas variantes, são alimentadas por um motor RL-10B2, fabricado pela Pratt & Whitney. (pt)
name	Delta Cryogenic Second Stage (en)
foaf:depiction
dcterms:subject	Delta (rocket family) Boeing spacecraft and space launch systems Rocket stages Rocket engines using hydrogen propellant United Launch Alliance Space Launch System
Wikipage page ID	30629936 (xsd:integer)
Wikipage revision ID	1122280200 (xsd:integer)
Link from a Wikipage to another Wikipage	Pratt & Whitney Multistage rocket Boeing Boeing Integrated Defense Systems Delta III Delta IV Delta IV Heavy United Launch Alliance Mitsubishi Heavy Industries Cryogenic fuel Liquid hydrogen Delta (rocket family) Boeing spacecraft and space launch systems Liquid oxygen Exploration Upper Stage Artemis 1 Rocket stages Aerojet Rocketdyne Rocket engines using hydrogen propellant United Launch Alliance Discovery Cube Orange County Artemis 4 Space Launch System Space Launch System RL10 RL-10 (rocket engine)
sameAs	Delta Cryogenic Second Stage Delta Cryogenic Second Stage Delta Cryogenic Second Stage Delta Cryogenic Second Stage Delta Cryogenic Second Stage Delta Cryogenic Second Stage Delta Cryogenic Second Stage Delta Cryogenic Second Stage Delta Cryogenic Second Stage Delta Cryogenic Second Stage Delta Cryogenic Second Stage Delta Cryogenic Second Stage
dbp:wikiPageUsesTemplate	dbt:Thor_and_Delta_rockets dbt:Asof dbt:Citation_needed dbt:Convert dbt:Image_frame dbt:Reflist dbt:Rocket-stub dbt:Short_description dbt:Use_American_English dbt:Infobox_rocket/Stage dbt:Upper_stages dbt:Infobox_rocket_stage
thumbnail	wiki-commons:Special:FilePath/Second_stage_of_a_Delta_IV_Medium_rocket.jpg?width=300
success	41 (xsd:integer) 240.0 (second) 300.0 (second)
align	center (en)
caption	A 4-meter DCSS from a Delta IV Medium (en) The Artemis 1 ICPS under construction (en)
content	400 (xsd:integer)
first	1998-08-27 (xsd:date)
last	TBD (en)
manufacturer	Boeing Boeing Integrated Defense Systems United Launch Alliance Mitsubishi Heavy Industries (en)
status	Active (en)
width	400 (xsd:integer)
has abstract	The Delta Cryogenic Second Stage (DCSS) is a family of cryogenic rocket stages used on the Delta III and Delta IV rockets, and on the Space Launch System Block 1. The stage consists of a cylindrical liquid hydrogen (LH2) tank structurally separated from an oblate spheroid liquid oxygen (LOX) tank. The LH2 tank cylinder carries payload launch loads, while the LOX tank and engine are suspended below within the rocket's inter-stage. The stage is powered by a single Aerojet Rocketdyne-Pratt & Whitney RL10B-2 engine, which features an extendable carbon-carbon nozzle to improve specific impulse. (en) Le Delta Cryogenic Second Stage (DCSS) est une famille d'étages supérieurs de fusée utilisée sur les lanceurs Delta III et Delta IV, et prévue d'être utilisée sur le lanceur lourd Space Launch System. (fr) Delta Cryogenic Second Stage (DCSS) adalah keluarga dari tahapan roket cryogenic digunakan pada roket delta III & Delta IV, dan yang rencananya akan digunakan pada Block I Space Launch System. Tahapan ini didukung oleh satu mesin Pratt & Whitney RL10B-2, yang memiliki nozzle karbon-karbon diperpanjang untuk meningkatkan dorongan tertentu. (in) Il Delta Cryogenic Second Stage (DCSS) è una famiglia di stadi a razzo criogenici usata sui veicoli di lancio Delta III e Delta IV e il cui utilizzo è previsto anche a bordo del Block 1 dello Space Launch System. Lo stadio consiste in un serbatoio cilindrico dell'idrogeno liquido strutturalmente separato da un serbatoio sferico dell'ossigeno liquido. Il cilindro del LH2 trasporta i carichi utili in ogni lancio, mentre il motore e il serbatoio LOX sono sospesi nell'interstadio del razzo. Lo stadio è alimentato da un singolo motore Pratt & Whitney RL10-B-2 fornito di un ugello al carbonio espandibile fornendo un elevato impulso specifico. (it)

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