AJ10-118G
From Spacefaring
model of hypergolic rocket engine
Wikidata
AJ-10-118G; Aerojet AJ10-118G
specific impulse by weight 314 second, maximum thrust 43.41 kilonewton,
Aerojet, United States,
United States, Ashkenaz, Calvinist Republic of Ghent, Chinland, Havilah, Kingdom of Martabam-hongsawatoi, Kingdom of Wolaita, Persia, Reman, Sikh Confederacy, Tarshish, Dong Fang Hong 2, Ekran, Republic of Haiti, liquid propellant rocket engine,
-
Location: KML, Cluster Map, Maps,
| Type | Subtype | Date | Description | Notes | Source |
|---|---|---|---|---|---|