R-4D-15 HiPAT

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Q135011540




model of hypergolic rocket engine

Wikidata
Aerojet R-4D-11 HiPAT; HiPAT; Marquardt R-4D-15 HiPAT; R4D-15 HiPAT
specific impulse by weight 322.2 second, length 70.57 centimetre, length 62.79 centimetre, diameter 36.2 centimetre, diameter 32.51 centimetre, maximum thrust 445 newton, mass 5.2 kilogram, mass 5.44 kilogram, 
R-4DAerojet Rocketdyne, United States
United StatesAshkenazCalvinist Republic of GhentChinlandHavilahKingdom of Martabam-hongsawatoiKingdom of WolaitaPersiaSikh ConfederacyTarshishDong Fang Hong 2R-4DRepublic of Haiti


Location: KML, Cluster Map, Maps,


      TypeSubtypeDateDescriptionNotesSource