Q31281956: Difference between revisions

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Q31281956
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{{Page|RL-10A-5|Classes|model of rocket engine}}
{{Page|RL-10A-5|Classes|model of rocket engine|RL10A-5}}

Latest revision as of 15:58, 17 February 2025




model of rocket engine

1993  Wikidata
RL10A-5
height 1.07 metre, mass 143 kilogram, diameter 1.02 metre, specific impulse by weight 316 second, maximum thrust 64.7 kilonewton, 
RL-10APratt & Whitney, United States
PersiaRepublic of Haiti1993RL-10AEkranDong Fang Hong 2TarshishSwedenSikh ConfederacyUnited StatesKingdom of WolaitaKingdom of Martabam-hongsawatoiHavilahDemocratic Republic of the CongoChinlandCalvinist Republic of GhentAshkenaz


Location: KML, Cluster Map, Maps,


      TypeSubtypeDateDescriptionNotesSource