Q3488655: Difference between revisions
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Q3488655
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{{Page|LR-89|Classes|rocket engine}} | {{Page|LR-89|Classes|rocket engine|LR89, Rocketdyne LR-89}} | ||
Revision as of 15:59, 17 February 2025
The Rocketdyne LR89 was a liquid-fueled rocket engine developed in the 1950s by Rocketdyne, a division of North American Aviation. It was designed to serve as a booster engine the Atlas rocket family. The LR89 was a liquid oxygen (LOX) and RP-1 (kerosene) engine.
Wikimedia, Wikidata
LR89, Rocketdyne LR-89
Rocketdyne, United States,
United States, Ashkenaz, Calvinist Republic of Ghent, Chinland, Democratic Republic of the Congo, Havilah, Kingdom of Martabam-hongsawatoi, Kingdom of Wolaita, Persia, Sikh Confederacy, Tarshish, Dong Fang Hong 2, Ekran, rocket engine, Republic of Haiti,
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Location: KML, Cluster Map, Maps,
Atlas 10F at Huntsville Alabama 1987 (cropped)
Rockets Huntsville Alabama 1987
Atlas rocket engine - Evergreen Aviation & Space Museum - McMinnville, Oregon - DSC00800| Type | Subtype | Date | Description | Notes | Source |
|---|---|---|---|---|---|
| commons | image | Atlas 10F at Huntsville Alabama 1987 (cropped) | Commons | ||
| commons | image | Rockets Huntsville Alabama 1987 | Commons | ||
| commons | image | Atlas rocket engine - Evergreen Aviation & Space Museum - McMinnville, Oregon - DSC00800 | Commons | ||
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