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- KTDU-35 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.".
- KTDU-35 wikiPageExternalLink main.php?id=53.
- KTDU-35 wikiPageID "47348378".
- KTDU-35 wikiPageLength "6195".
- KTDU-35 wikiPageOutDegree "43".
- KTDU-35 wikiPageRevisionID "703651959".
- KTDU-35 wikiPageWikiLink A.M._Isayev_Chemical_Engineering_Design_Bureau.
- KTDU-35 wikiPageWikiLink Aleksei_Isaev_(engineer).
- KTDU-35 wikiPageWikiLink Category:Rocket_engines_of_Russia.
- KTDU-35 wikiPageWikiLink Category:Rocket_engines_of_the_Soviet_Union.
- KTDU-35 wikiPageWikiLink Category:Rocket_engines_using_hypergolic_propellant.
- KTDU-35 wikiPageWikiLink Category:Spaceflight.
- KTDU-35 wikiPageWikiLink GRAU.
- KTDU-35 wikiPageWikiLink Gas-generator_cycle.
- KTDU-35 wikiPageWikiLink KTDU-80.
- KTDU-35 wikiPageWikiLink Kosmos_133.
- KTDU-35 wikiPageWikiLink Liquid-propellant_rocket.
- KTDU-35 wikiPageWikiLink Low_Earth_orbit.
- KTDU-35 wikiPageWikiLink Progress_(spacecraft).
- KTDU-35 wikiPageWikiLink Progress_7K-TG.
- KTDU-35 wikiPageWikiLink Red_fuming_nitric_acid.
- KTDU-35 wikiPageWikiLink Rocket_engine.
- KTDU-35 wikiPageWikiLink S5.4.
- KTDU-35 wikiPageWikiLink Salyut_1.
- KTDU-35 wikiPageWikiLink Salyut_4.
- KTDU-35 wikiPageWikiLink Soviet_Union.
- KTDU-35 wikiPageWikiLink Soviet_manned_lunar_programs.
- KTDU-35 wikiPageWikiLink Soyuz_(spacecraft).
- KTDU-35 wikiPageWikiLink Soyuz_7K-LOK.
- KTDU-35 wikiPageWikiLink Soyuz_7K-OK.
- KTDU-35 wikiPageWikiLink Soyuz_7K-OKS.
- KTDU-35 wikiPageWikiLink Soyuz_7K-T.
- KTDU-35 wikiPageWikiLink Soyuz_7K-TM.
- KTDU-35 wikiPageWikiLink Soyuz_programme.
- KTDU-35 wikiPageWikiLink Specific_impulse.
- KTDU-35 wikiPageWikiLink Unsymmetrical_dimethylhydrazine.
- KTDU-35 wikiPageWikiLinkText "KTDU-35".
- KTDU-35 burnTime "500.0".
- KTDU-35 chamberPressure "S5.60:".
- KTDU-35 combustionChamber "S5.35: 2".
- KTDU-35 combustionChamber "S5.60: 1".
- KTDU-35 countryOfOrigin Soviet_Union.
- KTDU-35 cycle Gas-generator_cycle.
- KTDU-35 date "1962".
- KTDU-35 designer "OKB-2, Anton Tavzarachvili".
- KTDU-35 firstDate "1966-11-28".
- KTDU-35 fuel Unsymmetrical_dimethylhydrazine.
- KTDU-35 mixtureRatio "1.85".
- KTDU-35 name "KTDU-35".
- KTDU-35 oxidiser Red_fuming_nitric_acid.
- KTDU-35 predecessor S5.4.
- KTDU-35 purpose "Spacecraft main propulsion".
- KTDU-35 restarts "25".
- KTDU-35 specificImpulseVacuum "270.0".
- KTDU-35 specificImpulseVacuum "278.0".
- KTDU-35 status "Retired".
- KTDU-35 successor KTDU-80.
- KTDU-35 thrust(vac)_ "S5.35:".
- KTDU-35 thrust(vac)_ "S5.60:".
- KTDU-35 type "liquid".
- KTDU-35 usedIn "Soyuz from 7K-OK to 7K-T and Progress 7K-TG".
- KTDU-35 wikiPageUsesTemplate Template:Convert.
- KTDU-35 wikiPageUsesTemplate Template:Infobox_rocket_engine.
- KTDU-35 wikiPageUsesTemplate Template:Orbital_spacecraft_rocket_engines.
- KTDU-35 wikiPageUsesTemplate Template:Reflist.
- KTDU-35 wikiPageUsesTemplate Template:Rocket-stub.
- KTDU-35 subject Category:Rocket_engines_of_Russia.
- KTDU-35 subject Category:Rocket_engines_of_the_Soviet_Union.
- KTDU-35 subject Category:Rocket_engines_using_hypergolic_propellant.
- KTDU-35 subject Category:Spaceflight.
- KTDU-35 hypernym System.
- KTDU-35 comment "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.".
- KTDU-35 label "KTDU-35".
- KTDU-35 sameAs Q20744071.
- KTDU-35 sameAs KTDU_35.
- KTDU-35 sameAs Q20744071.
- KTDU-35 wasDerivedFrom KTDU-35?oldid=703651959.
- KTDU-35 homepage main.php?id=53.
- KTDU-35 isPrimaryTopicOf KTDU-35.