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- S5.92 abstract "The S5.92, is a Russian rocket engine, currently powering the Fregat upper stages and it burns gas generator UDMH and nitrogen tetroxide. It has two throttle points. The first has 19.61 kilonewtons (4,410 lbf) of thrust, 327 seconds of isp, and 3 seconds of ignition transient. The second one has 13.73 kilonewtons (3,090 lbf) of thrust, 316 seconds of isp, and 2.5 seconds of ignition transient.It was designed by KB KhIMMASH, the famous Isaev Design Bureau, for the Phobos 1 and Phobos 2 Mars spacecrafts. As such, it is rated for 50 ignitions, and 300 days between ignitions. While the Mars missions where unsuccessful, the spacecraft manufacturer, NPO Lavochkin, found a market niche for most of the basic space vehicle technology. Thus, the basic vehicle was adapted as the Fregat upper stage for the Soyuz launch vehicle, and later for the Zenit. Since then, this engine has been performing very important scientific, commercial and military missions.".
- S5.92 wikiPageExternalLink main.php?id=53.
- S5.92 wikiPageExternalLink fregat.php.
- S5.92 wikiPageID "46876332".
- S5.92 wikiPageLength "4204".
- S5.92 wikiPageOutDegree "28".
- S5.92 wikiPageRevisionID "675950277".
- S5.92 wikiPageWikiLink A.M._Isayev_Chemical_Engineering_Design_Bureau.
- S5.92 wikiPageWikiLink Aleksei_Mihailovich_Isaev.
- S5.92 wikiPageWikiLink Category:Rocket_engines.
- S5.92 wikiPageWikiLink Category:Rocket_engines_of_Russia.
- S5.92 wikiPageWikiLink Category:Rocket_engines_of_the_Soviet_Union.
- S5.92 wikiPageWikiLink Category:Rocket_engines_using_hypergolic_propellant.
- S5.92 wikiPageWikiLink Category:Spaceflight.
- S5.92 wikiPageWikiLink Dinitrogen_tetroxide.
- S5.92 wikiPageWikiLink Fregat.
- S5.92 wikiPageWikiLink Gas-generator_cycle.
- S5.92 wikiPageWikiLink KB_KhIMMASH.
- S5.92 wikiPageWikiLink Lavochkin.
- S5.92 wikiPageWikiLink Mars.
- S5.92 wikiPageWikiLink N2O4.
- S5.92 wikiPageWikiLink Phobos_program.
- S5.92 wikiPageWikiLink Soviet_Union.
- S5.92 wikiPageWikiLink Soyuz_(rocket_family).
- S5.92 wikiPageWikiLink Spacecraft.
- S5.92 wikiPageWikiLink Spacecrafts.
- S5.92 wikiPageWikiLink UDMH.
- S5.92 wikiPageWikiLink USSR.
- S5.92 wikiPageWikiLink Unsymmetrical_dimethylhydrazine.
- S5.92 wikiPageWikiLink Zenit-3F.
- S5.92 wikiPageWikiLink Zenit_(rocket_family).
- S5.92 wikiPageWikiLinkText "S5.92".
- S5.92 associated Soyuz_(rocket_family).
- S5.92 associated Zenit_(rocket_family).
- S5.92 burnTime "2000.0".
- S5.92 combustionChamber "1".
- S5.92 countryOfOrigin Soviet_Union.
- S5.92 countryOfOrigin USSR.
- S5.92 cycle Gas-generator_cycle.
- S5.92 designer A.M._Isayev_Chemical_Engineering_Design_Bureau.
- S5.92 designer KB_KhIMMASH.
- S5.92 firstDate "1988-07-07".
- S5.92 fuel UDMH.
- S5.92 fuel Unsymmetrical_dimethylhydrazine.
- S5.92 hasPhotoCollection S5.92.
- S5.92 mixtureRatio "2".
- S5.92 name "S5.92".
- S5.92 oxidiser Dinitrogen_tetroxide.
- S5.92 oxidiser N2O4.
- S5.92 purpose "Upper Stage".
- S5.92 specificImpulseVacuum "327.0".
- S5.92 status "In Production".
- S5.92 type "liquid".
- S5.92 usedIn "Fregat and Phobos program".
- S5.92 wikiPageUsesTemplate Template:Convert.
- S5.92 wikiPageUsesTemplate Template:Infobox_rocket_engine.
- S5.92 wikiPageUsesTemplate Template:Orbital_spacecraft_rocket_engines.
- S5.92 wikiPageUsesTemplate Template:Reflist.
- S5.92 wikiPageUsesTemplate Template:Rocket-stub.
- S5.92 wikiPageUsesTemplate Template:Rocket_Engines.
- S5.92 subject Category:Rocket_engines.
- S5.92 subject Category:Rocket_engines_of_Russia.
- S5.92 subject Category:Rocket_engines_of_the_Soviet_Union.
- S5.92 subject Category:Rocket_engines_using_hypergolic_propellant.
- S5.92 subject Category:Spaceflight.
- S5.92 hypernym Engine.
- S5.92 type Software.
- S5.92 comment "The S5.92, is a Russian rocket engine, currently powering the Fregat upper stages and it burns gas generator UDMH and nitrogen tetroxide. It has two throttle points. The first has 19.61 kilonewtons (4,410 lbf) of thrust, 327 seconds of isp, and 3 seconds of ignition transient.".
- S5.92 label "S5.92".
- S5.92 sameAs m.013cc_js.
- S5.92 wasDerivedFrom S5.92?oldid=675950277.
- S5.92 homepage main.php?id=53.
- S5.92 isPrimaryTopicOf S5.92.