The Delta Cryogenic Second Stage (DCSS) is a family of cryogenic rocket stages used on the Delta III and Delta IV rockets, and which is planned to be used on the Space Launch System Block 1. The stage consists of a cylindrical LH2 tank structurally separated from an oblate spheroid 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 Pratt & Whitney RL10B-2 engine, which features an extendable carbon-carbon nozzle to improve specific impulse.

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dbo:abstract
  • 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)
  • The Delta Cryogenic Second Stage (DCSS) is a family of cryogenic rocket stages used on the Delta III and Delta IV rockets, and which is planned to be used on the Space Launch System Block 1. The stage consists of a cylindrical LH2 tank structurally separated from an oblate spheroid 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 Pratt & Whitney RL10B-2 engine, which features an extendable carbon-carbon nozzle to improve specific impulse. (en)
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  • A 4-meter DCSS from a Delta IV Medium (en)
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  • Delta Cryogenic Second Stage (en)
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  • 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)
  • The Delta Cryogenic Second Stage (DCSS) is a family of cryogenic rocket stages used on the Delta III and Delta IV rockets, and which is planned to be used on the Space Launch System Block 1. The stage consists of a cylindrical LH2 tank structurally separated from an oblate spheroid 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 Pratt & Whitney RL10B-2 engine, which features an extendable carbon-carbon nozzle to improve specific impulse. (en)
rdfs:label
  • Delta Cryogenic Second Stage (en)
  • Delta Cryogenic Second Stage (fr)
  • Delta Cryogenic Second Stage (in)
  • Delta Cryogenic Second Stage (it)
  • Delta Cryogenic Second Stage (pl)
  • Delta Cryogenic Second Stage (pt)
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