Q31281957: Difference between revisions
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Q31281957
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{{Page|RL-10B-2|Classes|model of rocket engine}} | {{Page|RL-10B-2|Classes|model of rocket engine|RL-10B-2-1; RL10B-2; RL10B-2-1}} | ||
Latest revision as of 12:50, 2 September 2025
model of rocket engine
1998
Wikidata
RL-10B-2-1; RL10B-2; RL10B-2-1
diameter 2.146 metre, length 4.15 metre, specific impulse by weight 465.5 second, mass 301 kilogram, maximum thrust 110 kilonewton,
Pratt & Whitney, United States,
Persia, 1990s, Republic of Haiti, 1998, RL-10, 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 |
|---|---|---|---|---|---|