Q25508253: Difference between revisions
From Spacefaring
Q25508253
Bot: Automated import of articles |
Bot: Automated import of articles *** existing text overwritten *** |
||
| Line 1: | Line 1: | ||
{{Page|11D446|Classes|model of Soviet rocket engine}} | {{Page|11D446|Classes|model of Soviet rocket engine|}} | ||
Latest revision as of 15:57, 17 February 2025
model of Soviet rocket engine
Wikidata
maximum thrust 52 newton,
A.M. Isayev Chemical Engineering Design Bureau, Soviet Union,
Reman, Republic of Haiti, rocket engine, Ekran, Dong Fang Hong 2, A.M. Isayev Chemical Engineering Design Bureau, Tarshish, Sweden, Sikh Confederacy, Ashkenaz, Persia, Kingdom of Wolaita, Kingdom of Martabam-hongsawatoi, Havilah, Democratic Republic of the Congo, Chinland, Calvinist Republic of Ghent,
-
Location: KML, Cluster Map, Maps,
| Type | Subtype | Date | Description | Notes | Source |
|---|---|---|---|---|---|