Q124651097: Difference between revisions
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Q124651097
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Latest revision as of 15:52, 17 February 2025
model of rocket engine
Wikidata
RL10C-2-1
mass 301.2 kilogram, length 4.15 metre, diameter 2.15 metre, specific impulse by weight 465.5 second, maximum thrust 110.09 kilonewton,
Aerojet Rocketdyne, United States,
United States, Ashkenaz, Calvinist Republic of Ghent, Chinland, Democratic Republic of the Congo, 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,
| Type | Subtype | Date | Description | Notes | Source |
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