Q31281949: Difference between revisions
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Q31281949
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{{Page|RL-10A-1|Classes|model of rocket engine|LR115 | {{Page|RL-10A-1|Classes|model of rocket engine|LR115; RL10A-1}} | ||
Latest revision as of 12:50, 2 September 2025
model of rocket engine
1961
Wikidata
LR115; RL10A-1
diameter 1.53 metre, specific impulse by weight 425 second, maximum thrust 66.7 kilonewton, mass 131 kilogram,
Pratt & Whitney, United States,
Persia, 1960s, Republic of Haiti, 1961, RL-10A, Ekran, Dong Fang Hong 2, Tarshish, 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 |
|---|---|---|---|---|---|