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|RL-10A-4-1B; RL10A-4-1; RL10A-4-1B}} | ||
Latest revision as of 12:50, 2 September 2025
model of rocket engine
2000
Wikidata
RL-10A-4-1B; RL10A-4-1; 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,
Persia, Republic of Haiti, 2000, RL-10A, Ekran, Dong Fang Hong 2, Tarshish, Sweden, Sikh Confederacy, United States, Kingdom of Wolaita, Kingdom of Martabam-hongsawatoi, Havilah, Democratic Republic of the Congo, Chinland, Calvinist Republic of Ghent, Ashkenaz,
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Location: KML, Cluster Map, Maps,
| Type | Subtype | Date | Description | Notes | Source |
|---|---|---|---|---|---|