Q6711969

The Aerojet M-1 was one of the largest and most powerful liquid-hydrogen-fueled liquid-fuel rocket engines to be designed and component-tested. It was originally developed during the 1950s by the US Air Force. The M-1 offered a baseline thrust of 1,500,000 pounds-force and an immediate growth target of 1,800,000 lb_f (8 MN). If built, the M-1 would have been larger and more efficient than the famed F-1 that powered the first stage of the Saturn V rocket to the Moon.

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M-1 (rocket engine)
rocket engine, Aerojet, 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,

Frameless

Rocket Engines Displayed for 1966 Inspection at Lewis Research Center

M-1 rocket engines Displayed for 1966 Inspection at Lewis Research Center (cropped)

Axial turbopump designed and built for the M-1 rocket engine

Type	Subtype	Date	Description	Notes	Source
commons	image		Rocket Engines Displayed for 1966 Inspection at Lewis Research Center		Commons
commons	image		M-1 rocket engines Displayed for 1966 Inspection at Lewis Research Center (cropped)		Commons
commons	image		Axial turbopump designed and built for the M-1 rocket engine		Commons