R-4D-11

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Q135011539




model of hypergolic rocket engine

Wikidata
Aerojet R-4D-11; Marquardt R-4D-11; R4D-11
specific impulse by weight 315.5 second, length 73.66 centimetre, length 31.67 centimetre, maximum thrust 490 newton, mass 4.31 kilogram, mass 3.76 kilogram, diameter 37.69 centimetre, diameter 15.26 centimetre, 
R-4DAerojet Rocketdyne, United States
United StatesAshkenazCalvinist Republic of GhentChinlandDemocratic Republic of the CongoHavilahKingdom of Martabam-hongsawatoiKingdom of WolaitaPersiaSikh ConfederacyTarshishDong Fang Hong 2EkranR-4DRepublic of Haiti


Location: KML, Cluster Map, Maps,


      TypeSubtypeDateDescriptionNotesSource