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- S5.80 abstract "The S5.80 is a liquid pressure-fed rocket engine burning N2O4/UDMH with an O/F of 1.85. It is used for crew-rated spacecraft propulsion applications. It is currently used in the Soyuz-TMA-M spacecraft propulsion module KTDU-80, and its sibling, the S5.79 rocket engine, is still used as the main propulsion of the Zvezda ISS module.The S5.80 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 engine, without the pressurization system or propellant tanks, weighs 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).".
- S5.80 wikiPageExternalLink main.php?id=53.
- S5.80 wikiPageID "47376249".
- S5.80 wikiPageLength "9827".
- S5.80 wikiPageOutDegree "73".
- S5.80 wikiPageRevisionID "703650767".
- S5.80 wikiPageWikiLink A.M._Isayev_Chemical_Engineering_Design_Bureau.
- S5.80 wikiPageWikiLink Category:Rocket_engines_of_Russia.
- S5.80 wikiPageWikiLink Category:Rocket_engines_of_the_Soviet_Union.
- S5.80 wikiPageWikiLink Category:Rocket_engines_using_hypergolic_propellant.
- S5.80 wikiPageWikiLink Category:Spaceflight.
- S5.80 wikiPageWikiLink Dinitrogen_tetroxide.
- S5.80 wikiPageWikiLink Human_spaceflight.
- S5.80 wikiPageWikiLink International_Space_Station.
- S5.80 wikiPageWikiLink KTDU-35.
- S5.80 wikiPageWikiLink KTDU-80.
- S5.80 wikiPageWikiLink Liquid-propellant_rocket.
- S5.80 wikiPageWikiLink Mir_Core_Module.
- S5.80 wikiPageWikiLink Pirs_(ISS_module).
- S5.80 wikiPageWikiLink Poisk_(ISS_module).
- S5.80 wikiPageWikiLink Pressure-fed_engine.
- S5.80 wikiPageWikiLink Progress-M.
- S5.80 wikiPageWikiLink Progress_(spacecraft).
- S5.80 wikiPageWikiLink Reaction_control_system.
- S5.80 wikiPageWikiLink Rocket_engine.
- S5.80 wikiPageWikiLink Rocket_propellant.
- S5.80 wikiPageWikiLink Roscosmos_State_Corporation.
- S5.80 wikiPageWikiLink S.P._Korolev_Rocket_and_Space_Corporation_Energia.
- S5.80 wikiPageWikiLink Salyut_6.
- S5.80 wikiPageWikiLink Salyut_7.
- S5.80 wikiPageWikiLink Salyut_programme.
- S5.80 wikiPageWikiLink Soviet_Union.
- S5.80 wikiPageWikiLink Soviet_space_program.
- S5.80 wikiPageWikiLink Soyuz-T.
- S5.80 wikiPageWikiLink Soyuz-TM.
- S5.80 wikiPageWikiLink Soyuz-TMA.
- S5.80 wikiPageWikiLink Soyuz_(spacecraft).
- S5.80 wikiPageWikiLink Soyuz_TM-1.
- S5.80 wikiPageWikiLink Spacecraft_propulsion.
- S5.80 wikiPageWikiLink Specific_impulse.
- S5.80 wikiPageWikiLink Unsymmetrical_dimethylhydrazine.
- S5.80 wikiPageWikiLink Zvezda_(ISS_module).
- S5.80 wikiPageWikiLinkText "S5.80".
- S5.80 burnTime "890.0".
- S5.80 combustionChamber "1".
- S5.80 countryOfOrigin Soviet_Union.
- S5.80 cycle Pressure-fed_engine.
- S5.80 date "1977".
- S5.80 designer "OKB-2, Anton Tavzarachvili".
- S5.80 firstDate "1986-05-21".
- S5.80 fuel Unsymmetrical_dimethylhydrazine.
- S5.80 gimbal "±5°".
- S5.80 mixtureRatio "1.85".
- S5.80 name "S5.80".
- S5.80 nozzleRatio "153.8".
- S5.80 oxidiser Dinitrogen_tetroxide.
- S5.80 predecessor "11".
- S5.80 purpose "Spacecraft main propulsion".
- S5.80 restarts "30".
- S5.80 status "In Production".
- S5.80 type "liquid".
- S5.80 usedIn "Soyuz since Soyuz-TM and Progress since Progress-M".
- S5.80 wikiPageUsesTemplate Template:Convert.
- S5.80 wikiPageUsesTemplate Template:Infobox_rocket_engine.
- S5.80 wikiPageUsesTemplate Template:Orbital_spacecraft_rocket_engines.
- S5.80 wikiPageUsesTemplate Template:Reflist.
- S5.80 subject Category:Rocket_engines_of_Russia.
- S5.80 subject Category:Rocket_engines_of_the_Soviet_Union.
- S5.80 subject Category:Rocket_engines_using_hypergolic_propellant.
- S5.80 subject Category:Spaceflight.
- S5.80 hypernym UDMH.
- S5.80 comment "The S5.80 is a liquid pressure-fed rocket engine burning N2O4/UDMH with an O/F of 1.85. It is used for crew-rated spacecraft propulsion applications.".
- S5.80 label "S5.80".
- S5.80 sameAs Q13288017.
- S5.80 sameAs KRD_79.
- S5.80 sameAs Q13288017.
- S5.80 wasDerivedFrom S5.80?oldid=703650767.
- S5.80 homepage main.php?id=53.
- S5.80 isPrimaryTopicOf S5.80.