Q31281953: Difference between revisions
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Q31281953
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Latest revision as of 15:58, 17 February 2025
model of rocket engine
1992
Wikidata
RL10A-4
diameter 1.17 metre, height 2.29 metre, specific impulse by weight 449 second, mass 168 kilogram, maximum thrust 92.5 kilonewton,
Pratt & Whitney, United States,
Sikh Confederacy, 1990s, Republic of Haiti, 1992, RL-10A, Ekran, Dong Fang Hong 2, Tarshish, Sweden, United States, Persia, 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 |
|---|---|---|---|---|---|