Q4803858: Difference between revisions
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Q4803858
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{{Page|Ascent Propulsion System|Classes|rocket engine used by the Apollo Lunar Module}} | {{Page|Ascent Propulsion System|Classes|rocket engine used by the Apollo Lunar Module|APS, LMAE, Lunar Module Ascent Engine}} | ||
Revision as of 16:01, 17 February 2025
The ascent propulsion system (APS) or lunar module ascent engine (LMAE) is a fixed-thrust hypergolic rocket engine developed by Bell Aerosystems for use in the Apollo Lunar Module ascent stage. It used Aerozine 50 fuel, and N
2O
4 oxidizer. Rocketdyne provided the injector system, at the request of NASA, when Bell could not solve combustion instability problems.
Wikimedia, Wikidata
APS, LMAE, Lunar Module Ascent Engine
Bell Aircraft Corporation, 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, rocket engine, Republic of Haiti,
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Location: KML, Cluster Map, Maps,
Apollo Lunar Module Ascent Engine
View of O&C Building Altitude Chambers
Lunar module ascent engine| Type | Subtype | Date | Description | Notes | Source |
|---|---|---|---|---|---|
| commons | image | Apollo Lunar Module Ascent Engine | Commons | ||
| commons | image | View of O&C Building Altitude Chambers | Commons | ||
| commons | image | Lunar module ascent engine | Commons | ||
.jpg){kind=link}
