Q31281950: Difference between revisions
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Q31281950
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{{Page|RL-10A-3A|Classes|model of rocket engine|RL-10A-3-3A | {{Page|RL-10A-3A|Classes|model of rocket engine|RL-10A-3-3A; RL10A-3-3A; RL10A-3A}} | ||
Latest revision as of 12:50, 2 September 2025
model of rocket engine
1984
Wikidata
RL-10A-3-3A; RL10A-3-3A; RL10A-3A
height 1.78 metre, diameter 1.01 metre, mass 141 kilogram, specific impulse by weight 444 second, maximum thrust 73.4 kilonewton,
Pratt & Whitney,
Persia, 1980s, Republic of Haiti, 1984, 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 |
|---|---|---|---|---|---|