Q31281954: Difference between revisions
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Q31281954
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{{Page|RL-10A-4-1|Classes|model of rocket engine}} | {{Page|RL-10A-4-1|Classes|model of rocket engine|RL10A-4-1, RL-10A-4-1B, RL10A-4-1B}} | ||
Revision as of 15:58, 17 February 2025
model of rocket engine
2000
Wikidata
RL10A-4-1, RL-10A-4-1B, RL10A-4-1B
maximum thrust 99.1 kilonewton, diameter 1.53 metre, specific impulse by weight 451 second, mass 167 kilogram,
Pratt & Whitney, 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-10A, 2000, Republic of Haiti,
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Location: KML, Cluster Map, Maps,
| Type | Subtype | Date | Description | Notes | Source |
|---|---|---|---|---|---|