Q124651098: Difference between revisions
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Q124651098
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Revision as of 20:15, 30 August 2024
model of rocket engine
Wikidata
diameter 1.85 metre, length 3.16 metre, mass 230.4 kilogram, specific impulse by weight 460.1 second, maximum thrust 108.27 kilonewton,
Aerojet Rocketdyne, United States,
United States, Ashkenaz, Calvinist Republic of Ghent, Chinland, Havilah, Kingdom of Martabam-hongsawatoi, Kingdom of Wolaita, Persia, Sikh Confederacy, Tarshish, Dong Fang Hong 2, Ekran, RL-10C, Republic of Haiti,
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Location: KML, Cluster Map, Maps,
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