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- Aestus abstract "Aestus is a hypergolic liquid rocket engine used on an upper stage of Ariane 5 family rockets for the orbital insertion. It features unique design of 132 coaxial injection elements causing swirl mixing of the MMH propellants with Nitrogen tetroxide oxidizer. Engine allows for multiple re-ignitions.".
- Aestus wikiPageID "43317149".
- Aestus wikiPageLength "6186".
- Aestus wikiPageOutDegree "44".
- Aestus wikiPageRevisionID "698329186".
- Aestus wikiPageWikiLink Airbus_Defence_and_Space.
- Aestus wikiPageWikiLink Ariane_5.
- Aestus wikiPageWikiLink Ariane_6.
- Aestus wikiPageWikiLink Astrium.
- Aestus wikiPageWikiLink Automated_Transfer_Vehicle.
- Aestus wikiPageWikiLink Bar_(unit).
- Aestus wikiPageWikiLink Category:Rocket_engines.
- Aestus wikiPageWikiLink Category:Rocket_engines_using_hypergolic_propellant.
- Aestus wikiPageWikiLink Category:Spacecraft_propulsion.
- Aestus wikiPageWikiLink Dinitrogen_tetroxide.
- Aestus wikiPageWikiLink European_Space_Agency.
- Aestus wikiPageWikiLink Germany.
- Aestus wikiPageWikiLink Hypergolic_propellant.
- Aestus wikiPageWikiLink Jules_Verne_ATV.
- Aestus wikiPageWikiLink Liquid-propellant_rocket.
- Aestus wikiPageWikiLink Monomethylhydrazine.
- Aestus wikiPageWikiLink Multistage_rocket.
- Aestus wikiPageWikiLink Orbit_insertion.
- Aestus wikiPageWikiLink Pratt_&_Whitney_Rocketdyne.
- Aestus wikiPageWikiLink Pressure-fed_engine.
- Aestus wikiPageWikiLink United_States.
- Aestus wikiPageWikiLink White_Sands_Test_Facility.
- Aestus wikiPageWikiLinkText "Aestus".
- Aestus wikiPageWikiLinkText "Aestus#Aestus II / RS-72".
- Aestus associated European_Space_Agency.
- Aestus burnTime "1100.0".
- Aestus burnTime "600.0".
- Aestus chamberPressure "11.0".
- Aestus chamberPressure "60.0".
- Aestus countryOfOrigin Germany.
- Aestus countryOfOrigin United_States.
- Aestus cycle Pressure-fed_engine.
- Aestus designer Airbus_Defence_and_Space.
- Aestus designer Pratt_&_Whitney_Rocketdyne.
- Aestus diameter "1.31 m".
- Aestus dryWeight "111.0".
- Aestus dryWeight "138.0".
- Aestus firstDate "1997-10-30".
- Aestus fuel Monomethylhydrazine.
- Aestus length "2.20 m".
- Aestus length "2.29 m".
- Aestus manufacturer Astrium.
- Aestus manufacturer Pratt_&_Whitney_Rocketdyne.
- Aestus mixtureRatio "19".
- Aestus name "Aestus II / RS-72".
- Aestus name "Aestus".
- Aestus nozzleRatio "84".
- Aestus oxidiser Dinitrogen_tetroxide.
- Aestus predecessor "Aestus".
- Aestus pumps "XLR-132".
- Aestus purpose "Upper stage engine for the orbital insertion of heavy payloads".
- Aestus status "In development".
- Aestus status "In use".
- Aestus successor "Aestus II".
- Aestus type "liquid".
- Aestus usedIn "Ariane 5 G and ES".
- Aestus usedIn "Ariane 6.1".
- Aestus wikiPageUsesTemplate Template:Ariane.
- Aestus wikiPageUsesTemplate Template:Convert.
- Aestus wikiPageUsesTemplate Template:Infobox_rocket_engine.
- Aestus wikiPageUsesTemplate Template:Reflist.
- Aestus wikiPageUsesTemplate Template:Rocket_Engines.
- Aestus subject Category:Rocket_engines.
- Aestus subject Category:Rocket_engines_using_hypergolic_propellant.
- Aestus subject Category:Spacecraft_propulsion.
- Aestus hypernym Engine.
- Aestus type Software.
- Aestus comment "Aestus is a hypergolic liquid rocket engine used on an upper stage of Ariane 5 family rockets for the orbital insertion. It features unique design of 132 coaxial injection elements causing swirl mixing of the MMH propellants with Nitrogen tetroxide oxidizer. Engine allows for multiple re-ignitions.".
- Aestus label "Aestus".
- Aestus sameAs Q16840.
- Aestus sameAs Aestus.
- Aestus sameAs Aestus.
- Aestus sameAs Aestus.
- Aestus sameAs エスタス_(ロケットエンジン).
- Aestus sameAs Aestus.
- Aestus sameAs Aestus.
- Aestus sameAs m.05sp7jj.
- Aestus sameAs Q16840.
- Aestus wasDerivedFrom Aestus?oldid=698329186.
- Aestus isPrimaryTopicOf Aestus.