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- 11D428 abstract "The 11D428A-16 (manufacturer's name RDMT-135M) 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 KTDU-80 spacecraft propulsion module. The previous version, the 11D428A (manufacturer's name RDMT-135) is still used as the reaction control system thrusters of the Zvezda ISS module.The 11D428A-16 generates 129.16 N (29.04 lbf) of thrust with a chamber pressure of 0.88 MPa (128 psi) and achieves a specific impulse of 291 s (2.85 km/s). It is rated for 500,000 starts with a certified ignition time of 0.03 seconds to 2000 seconds. Each unit weights 1.5 kg (3.3 lb).".
- 11D428 wikiPageExternalLink main.php?id=53.
- 11D428 wikiPageID "47397855".
- 11D428 wikiPageLength "8464".
- 11D428 wikiPageOutDegree "64".
- 11D428 wikiPageRevisionID "675949143".
- 11D428 wikiPageWikiLink A.M._Isayev_Chemical_Engineering_Design_Bureau.
- 11D428 wikiPageWikiLink Category:Rocket_engines_of_Russia.
- 11D428 wikiPageWikiLink Category:Rocket_engines_of_the_Soviet_Union.
- 11D428 wikiPageWikiLink Category:Rocket_engines_using_hypergolic_propellant.
- 11D428 wikiPageWikiLink Category:Spaceflight.
- 11D428 wikiPageWikiLink Dinitrogen_tetroxide.
- 11D428 wikiPageWikiLink Federal_State_Unitary_Enterprise_Research_and_Development_Institute_of_Mechanical_Engineering.
- 11D428 wikiPageWikiLink Fobos-Grunt.
- 11D428 wikiPageWikiLink Human_spaceflight.
- 11D428 wikiPageWikiLink International_Space_Station.
- 11D428 wikiPageWikiLink KB_KhIMMASH.
- 11D428 wikiPageWikiLink KTDU-35.
- 11D428 wikiPageWikiLink KTDU-426.
- 11D428 wikiPageWikiLink KTDU-80.
- 11D428 wikiPageWikiLink Kosmos_670.
- 11D428 wikiPageWikiLink Kosmos_697.
- 11D428 wikiPageWikiLink Kosmos_772.
- 11D428 wikiPageWikiLink Kosmos_869.
- 11D428 wikiPageWikiLink Liquid-propellant_rocket.
- 11D428 wikiPageWikiLink Mir_Core_Module.
- 11D428 wikiPageWikiLink Pressure-fed_engine.
- 11D428 wikiPageWikiLink Progress_(spacecraft).
- 11D428 wikiPageWikiLink Progress_M-36.
- 11D428 wikiPageWikiLink Reaction_control_system.
- 11D428 wikiPageWikiLink Rocket_engine.
- 11D428 wikiPageWikiLink Rocket_propellant.
- 11D428 wikiPageWikiLink Russia.
- 11D428 wikiPageWikiLink Russian_Federal_Space_Agency.
- 11D428 wikiPageWikiLink Russian_space_program.
- 11D428 wikiPageWikiLink Salyut-6.
- 11D428 wikiPageWikiLink Salyut-7.
- 11D428 wikiPageWikiLink Salyut_1.
- 11D428 wikiPageWikiLink Salyut_6.
- 11D428 wikiPageWikiLink Salyut_7.
- 11D428 wikiPageWikiLink Soviet_space_program.
- 11D428 wikiPageWikiLink Soyuz-T.
- 11D428 wikiPageWikiLink Soyuz-TM.
- 11D428 wikiPageWikiLink Soyuz-TMA.
- 11D428 wikiPageWikiLink Soyuz_(spacecraft).
- 11D428 wikiPageWikiLink Soyuz_7K-S.
- 11D428 wikiPageWikiLink Soyuz_TM-28.
- 11D428 wikiPageWikiLink Spacecraft_propulsion.
- 11D428 wikiPageWikiLink Specific_impulse.
- 11D428 wikiPageWikiLink Unsymmetrical_dimethylhydrazine.
- 11D428 wikiPageWikiLink Yantar-2K.
- 11D428 wikiPageWikiLink Zvezda_(ISS_module).
- 11D428 wikiPageWikiLinkText "11D428".
- 11D428 wikiPageWikiLinkText "11D428A-16".
- 11D428 combustionChamber "1".
- 11D428 countryOfOrigin Russia.
- 11D428 cycle Pressure-fed_engine.
- 11D428 date "1993".
- 11D428 designer Federal_State_Unitary_Enterprise_Research_and_Development_Institute_of_Mechanical_Engineering.
- 11D428 firstDate "1997-10-05".
- 11D428 fuel Unsymmetrical_dimethylhydrazine.
- 11D428 hasPhotoCollection 11D428.
- 11D428 mixtureRatio "1.85".
- 11D428 name "11".
- 11D428 oxidiser Dinitrogen_tetroxide.
- 11D428 predecessor "11".
- 11D428 purpose "RCS thruster".
- 11D428 restarts "500000".
- 11D428 status "In Production".
- 11D428 successor "11".
- 11D428 type "liquid".
- 11D428 usedIn "Soyuz since Soyuz TM-28 and Progress since Progress M-36".
- 11D428 wikiPageUsesTemplate Template:Convert.
- 11D428 wikiPageUsesTemplate Template:Infobox_rocket_engine.
- 11D428 wikiPageUsesTemplate Template:Orbital_spacecraft_rocket_engines.
- 11D428 wikiPageUsesTemplate Template:Reflist.
- 11D428 subject Category:Rocket_engines_of_Russia.
- 11D428 subject Category:Rocket_engines_of_the_Soviet_Union.
- 11D428 subject Category:Rocket_engines_using_hypergolic_propellant.
- 11D428 subject Category:Spaceflight.
- 11D428 hypernym UDMH.
- 11D428 comment "The 11D428A-16 (manufacturer's name RDMT-135M) 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 KTDU-80 spacecraft propulsion module.".
- 11D428 label "11D428".
- 11D428 sameAs 11D428.
- 11D428 sameAs Q12379756.
- 11D428 sameAs Q12379756.
- 11D428 wasDerivedFrom 11D428?oldid=675949143.
- 11D428 homepage main.php?id=53.
- 11D428 isPrimaryTopicOf 11D428.