Q11686315: Difference between revisions

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Q11686315
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{{Page|Antares 1A|Classes|retired American solid propellant rocket stage}}
{{Page|Antares 1A|Classes|retired American solid propellant rocket stage|}}

Latest revision as of 12:58, 17 February 2025




retired American solid propellant rocket stage

1960 — 1970  Wikidata
specific impulse by weight 256 second, mass 1225 kilogram, diameter 0.78 metre, height 3.38 metre, maximum thrust 60.5 kilonewton, 
rocket stage, solid-propellant rocket, United States
United StatesAshkenazCalvinist Republic of GhentChinlandHavilahKingdom of Martabam-hongsawatoiKingdom of WolaitaPersiaRemanSikh ConfederacyTarshishDong Fang Hong 2Ekran1960Republic of Haiti1960s


Location: KML, Cluster Map, Maps,


      TypeSubtypeDateDescriptionNotesSource