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About: KTDU-35

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The KTDU-35 (GRAU Index 11D62) was a Soviet spacecraft propulsion system composed of two liquid rocket engines, the primary, S5.60 (SKD) and the secondary S5.35 (DKD), fed from the same propellant tanks. Both engines burn UDMH and AK27I in the gas generator cycle. It was designed by OKB-2, the famous Isaev Design Bureau, for the original Soyuz programme.

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dbo:abstract
  • The KTDU-35 (GRAU Index 11D62) was a Soviet spacecraft propulsion system composed of two liquid rocket engines, the primary, S5.60 (SKD) and the secondary S5.35 (DKD), fed from the same propellant tanks. Both engines burn UDMH and AK27I in the gas generator cycle. It was designed by OKB-2, the famous Isaev Design Bureau, for the original Soyuz programme. Within the Soyuz and Progress, the SKD is the primary engine, the DKD is the backup engine for main orbital correction and de-orbit operations. The engine generate 4.09 kN (920 lbf) (SKD) or 4.03 kN (910 lbf) (DKD) of thrust with a specific impulse of 278 seconds and 270 seconds, respectively. The SKD nozzle is fixed in the aft of the craft, and the dual DKD nozzles are on either side. The spacecraft attitude system (DPO) is responsible for pointing the vehicle in the correct direction and keep it that way during SKD burns. (en)
  • O KTDU-35 (também conhecido como 11D62), foi um sistema de propulsão soviético, composto por dois motores de foguete a combustível líquido. O primário S5.60 (SKD) e o secundário S5.35 (DKD), abastecidos pelos mesmos tanques queimando UDMH e AK27I num ciclo de geração de gás. Ele foi projetado por e desenvolvido no para o Programa Soyuz. (pt)
dbo:wikiPageExternalLink
dbo:wikiPageID
  • 47348378 (xsd:integer)
dbo:wikiPageLength
  • 6621 (xsd:nonNegativeInteger)
dbo:wikiPageRevisionID
  • 1084020183 (xsd:integer)
dbo:wikiPageWikiLink
dbp:burnTime
  • 500.0 (dbd:second)
dbp:chamberPressure
  • S5.60: (en)
dbp:combustionChamber
  • S5.35: 2 (en)
  • S5.60: 1 (en)
dbp:countryOfOrigin
dbp:cycle
dbp:date
  • 1962 (xsd:integer)
dbp:designer
  • OKB-2, Anton Tavzarachvili (en)
dbp:firstDate
  • 1966-11-28 (xsd:date)
dbp:fuel
dbp:mixtureRatio
  • 1.850000 (xsd:double)
dbp:name
  • KTDU-35 (en)
dbp:oxidiser
dbp:predecessor
dbp:purpose
  • Spacecraft main propulsion (en)
dbp:restarts
  • 25 (xsd:integer)
dbp:specificImpulseVacuum
  • 270.0 (dbd:second)
  • 278.0 (dbd:second)
dbp:status
  • Retired (en)
dbp:successor
dbp:thrust(vac)_
  • S5.35: (en)
  • S5.60: (en)
dbp:type
  • liquid (en)
dbp:usedIn
  • Soyuz from 7K-OK to 7K-T and Progress 7K-TG (en)
dbp:wikiPageUsesTemplate
dct:subject
gold:hypernym
rdfs:comment
  • O KTDU-35 (também conhecido como 11D62), foi um sistema de propulsão soviético, composto por dois motores de foguete a combustível líquido. O primário S5.60 (SKD) e o secundário S5.35 (DKD), abastecidos pelos mesmos tanques queimando UDMH e AK27I num ciclo de geração de gás. Ele foi projetado por e desenvolvido no para o Programa Soyuz. (pt)
  • The KTDU-35 (GRAU Index 11D62) was a Soviet spacecraft propulsion system composed of two liquid rocket engines, the primary, S5.60 (SKD) and the secondary S5.35 (DKD), fed from the same propellant tanks. Both engines burn UDMH and AK27I in the gas generator cycle. It was designed by OKB-2, the famous Isaev Design Bureau, for the original Soyuz programme. (en)
rdfs:label
  • KTDU-35 (en)
  • KTDU-35 (pt)
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