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- KTDU-80 abstract "The KTDU-80 (Russian: Корректирующе-Тормозная Двигательная Установка, КТДУ) is the latest of a family of integrated propulsion system that KB KhIMMASH has implemented for the Soyuz since the Soyuz-T. It integrates main propulsion, RCS and attitude control in a single system pressure fed from a common dual string redundant pressurized propellant system. The common propellant is UDMH and N2O4 and the main propulsion unit, is the S5.80 main engine. It generates 2.95 kN (660 lbf) of thrust with a chamber pressure of 0.88 MPa (128 psi) and a nozzle expansion of 153.8 that enables it to achieve a specific impulse of 302 s (2.96 km/s). It is rated for 30 starts with a total firing time of 890 seconds. The integrated system without the pressurization nor tanks weights 310 kg (680 lb) and is an integrated unit that is 1.2 m (47 in) long with a diameter of 2.1 m (83 in).".
- KTDU-80 thumbnail Soyuz_TM-32.jpg?width=300.
- KTDU-80 wikiPageExternalLink main.php?id=53.
- KTDU-80 wikiPageID "47368374".
- KTDU-80 wikiPageLength "20914".
- KTDU-80 wikiPageOutDegree "109".
- KTDU-80 wikiPageRevisionID "675949351".
- KTDU-80 wikiPageWikiLink 11D426.
- KTDU-80 wikiPageWikiLink 11D428.
- KTDU-80 wikiPageWikiLink 11D428A.
- KTDU-80 wikiPageWikiLink 11D428A-16.
- KTDU-80 wikiPageWikiLink A.M._Isayev_Chemical_Engineering_Design_Bureau.
- KTDU-80 wikiPageWikiLink Aleksei_Mihailovich_Isaev.
- KTDU-80 wikiPageWikiLink Attitude_control.
- KTDU-80 wikiPageWikiLink Catalysis.
- KTDU-80 wikiPageWikiLink Category:Rocket_engines_of_Russia.
- KTDU-80 wikiPageWikiLink Category:Rocket_engines_of_the_Soviet_Union.
- KTDU-80 wikiPageWikiLink Category:Rocket_engines_using_hypergolic_propellant.
- KTDU-80 wikiPageWikiLink Category:Spaceflight.
- KTDU-80 wikiPageWikiLink Dinitrogen_tetroxide.
- KTDU-80 wikiPageWikiLink Electro-hydraulic_actuator.
- KTDU-80 wikiPageWikiLink Federal_State_Unitary_Enterprise_Research_and_Development_Institute_of_Mechanical_Engineering.
- KTDU-80 wikiPageWikiLink GRAU.
- KTDU-80 wikiPageWikiLink Gas-generator_cycle.
- KTDU-80 wikiPageWikiLink Gimbal.
- KTDU-80 wikiPageWikiLink Helium.
- KTDU-80 wikiPageWikiLink Hydrogen_peroxide.
- KTDU-80 wikiPageWikiLink International_Space_Station.
- KTDU-80 wikiPageWikiLink KB_KhIMMASH.
- KTDU-80 wikiPageWikiLink KTDU-35.
- KTDU-80 wikiPageWikiLink Monopropellant_rocket.
- KTDU-80 wikiPageWikiLink Pressure-fed_engine.
- KTDU-80 wikiPageWikiLink Progress-M.
- KTDU-80 wikiPageWikiLink Progress_M-36.
- KTDU-80 wikiPageWikiLink Progress_M-37.
- KTDU-80 wikiPageWikiLink Progress_M-38.
- KTDU-80 wikiPageWikiLink Progress_M-39.
- KTDU-80 wikiPageWikiLink Reaction_control_system.
- KTDU-80 wikiPageWikiLink Red_fuming_nitric_acid.
- KTDU-80 wikiPageWikiLink Rocket_engine.
- KTDU-80 wikiPageWikiLink Russian_language.
- KTDU-80 wikiPageWikiLink S.P._Korolev_Rocket_and_Space_Corporation_Energia.
- KTDU-80 wikiPageWikiLink S5.142.
- KTDU-80 wikiPageWikiLink S5.35.
- KTDU-80 wikiPageWikiLink S5.60.
- KTDU-80 wikiPageWikiLink S5.79.
- KTDU-80 wikiPageWikiLink S5.80.
- KTDU-80 wikiPageWikiLink Soyuz-MS.
- KTDU-80 wikiPageWikiLink Soyuz-T.
- KTDU-80 wikiPageWikiLink Soyuz-TM.
- KTDU-80 wikiPageWikiLink Soyuz-TMA.
- KTDU-80 wikiPageWikiLink Soyuz-TMA-M.
- KTDU-80 wikiPageWikiLink Soyuz_(spacecraft).
- KTDU-80 wikiPageWikiLink Soyuz_7K-OK.
- KTDU-80 wikiPageWikiLink Soyuz_7K-T.
- KTDU-80 wikiPageWikiLink Soyuz_TM-23.
- KTDU-80 wikiPageWikiLink Soyuz_TM-28.
- KTDU-80 wikiPageWikiLink Soyuz_TMA-11M.
- KTDU-80 wikiPageWikiLink Soyuz_TMA-4.
- KTDU-80 wikiPageWikiLink Soyuz_TMA-5.
- KTDU-80 wikiPageWikiLink Specific_impulse.
- KTDU-80 wikiPageWikiLink Squib_(explosive).
- KTDU-80 wikiPageWikiLink Unsymmetrical_dimethylhydrazine.
- KTDU-80 wikiPageWikiLink File:Soyuz_TM-32.jpg.
- KTDU-80 wikiPageWikiLinkText "KTDU-80".
- KTDU-80 hasPhotoCollection KTDU-80.
- KTDU-80 wikiPageUsesTemplate Template:Convert.
- KTDU-80 wikiPageUsesTemplate Template:Orbital_spacecraft_rocket_engines.
- KTDU-80 wikiPageUsesTemplate Template:Reflist.
- KTDU-80 subject Category:Rocket_engines_of_Russia.
- KTDU-80 subject Category:Rocket_engines_of_the_Soviet_Union.
- KTDU-80 subject Category:Rocket_engines_using_hypergolic_propellant.
- KTDU-80 subject Category:Spaceflight.
- KTDU-80 comment "The KTDU-80 (Russian: Корректирующе-Тормозная Двигательная Установка, КТДУ) is the latest of a family of integrated propulsion system that KB KhIMMASH has implemented for the Soyuz since the Soyuz-T. It integrates main propulsion, RCS and attitude control in a single system pressure fed from a common dual string redundant pressurized propellant system. The common propellant is UDMH and N2O4 and the main propulsion unit, is the S5.80 main engine.".
- KTDU-80 label "KTDU-80".
- KTDU-80 sameAs KTDU_80.
- KTDU-80 sameAs Q20744072.
- KTDU-80 sameAs Q20744072.
- KTDU-80 wasDerivedFrom KTDU-80?oldid=675949351.
- KTDU-80 depiction Soyuz_TM-32.jpg.
- KTDU-80 homepage main.php?id=53.
- KTDU-80 isPrimaryTopicOf KTDU-80.