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- S5.98M abstract "The S5.98M, also known as the 14D30, is a Russian rocket engine, currently powering the Briz upper stages. It was designed by KB KhIMMASH, the famous Isaev designed bureau, and it burns closed cycle UDMH and nitrogen tetroxide.".
- S5.98M thumbnail С5.98.jpg?width=300.
- S5.98M wikiPageExternalLink main.php?id=52.
- S5.98M wikiPageExternalLink main.php?id=49&lang=en.
- S5.98M wikiPageExternalLink www.eurockot.com.
- S5.98M wikiPageExternalLink breeze-m.
- S5.98M wikiPageID "38033621".
- S5.98M wikiPageLength "4447".
- S5.98M wikiPageOutDegree "24".
- S5.98M wikiPageRevisionID "691776778".
- S5.98M wikiPageWikiLink A.M._Isayev_Chemical_Engineering_Design_Bureau.
- S5.98M wikiPageWikiLink Aleksei_Isaev_(engineer).
- S5.98M wikiPageWikiLink Briz-M.
- S5.98M wikiPageWikiLink Category:Rocket_engines.
- S5.98M wikiPageWikiLink Category:Rocket_engines_of_Russia.
- S5.98M wikiPageWikiLink Category:Rocket_engines_of_the_Soviet_Union.
- S5.98M wikiPageWikiLink Category:Rocket_engines_using_hypergolic_propellant.
- S5.98M wikiPageWikiLink Category:Spaceflight.
- S5.98M wikiPageWikiLink Dinitrogen_tetroxide.
- S5.98M wikiPageWikiLink Khrunichev_State_Research_and_Production_Space_Center.
- S5.98M wikiPageWikiLink Proton-M.
- S5.98M wikiPageWikiLink Rokot.
- S5.98M wikiPageWikiLink Russia.
- S5.98M wikiPageWikiLink Staged_combustion_cycle.
- S5.98M wikiPageWikiLink Unsymmetrical_dimethylhydrazine.
- S5.98M wikiPageWikiLinkText "S5.98M".
- S5.98M associated "Proton-M and Rokot".
- S5.98M burnTime "3200.0".
- S5.98M combustionChamber "1".
- S5.98M countryOfOrigin Russia.
- S5.98M cycle Staged_combustion_cycle.
- S5.98M firstDate "1990-11-20".
- S5.98M fuel Unsymmetrical_dimethylhydrazine.
- S5.98M manufacturer A.M._Isayev_Chemical_Engineering_Design_Bureau.
- S5.98M mixtureRatio "2".
- S5.98M name "S5.98M".
- S5.98M oxidiser Dinitrogen_tetroxide.
- S5.98M predecessor "none".
- S5.98M purpose "Upper Stage".
- S5.98M restarts "7".
- S5.98M specificImpulseVacuum "328.6".
- S5.98M status "In Production".
- S5.98M type "liquid".
- S5.98M usedIn "Briz-M and Rokot".
- S5.98M wikiPageUsesTemplate Template:Convert.
- S5.98M wikiPageUsesTemplate Template:Infobox_rocket_engine.
- S5.98M wikiPageUsesTemplate Template:Reflist.
- S5.98M wikiPageUsesTemplate Template:Rocket-stub.
- S5.98M wikiPageUsesTemplate Template:Rocket_Engines.
- S5.98M subject Category:Rocket_engines.
- S5.98M subject Category:Rocket_engines_of_Russia.
- S5.98M subject Category:Rocket_engines_of_the_Soviet_Union.
- S5.98M subject Category:Rocket_engines_using_hypergolic_propellant.
- S5.98M subject Category:Spaceflight.
- S5.98M hypernym Engine.
- S5.98M type Software.
- S5.98M comment "The S5.98M, also known as the 14D30, is a Russian rocket engine, currently powering the Briz upper stages. It was designed by KB KhIMMASH, the famous Isaev designed bureau, and it burns closed cycle UDMH and nitrogen tetroxide.".
- S5.98M label "S5.98M".
- S5.98M sameAs Q4402922.
- S5.98M sameAs S5.98M.
- S5.98M sameAs m.0pclsb7.
- S5.98M sameAs С5.98М_(ЖРД).
- S5.98M sameAs Q4402922.
- S5.98M wasDerivedFrom S5.98M?oldid=691776778.
- S5.98M depiction С5.98.jpg.
- S5.98M homepage main.php?id=52.
- S5.98M isPrimaryTopicOf S5.98M.