Reaction Motors XLR11

The XLR11, company designation RMI 6000C4, was the first liquid-propellant rocket engine developed in the United States for use in aircraft. It was designed and built by Reaction Motors Inc., and used ethyl alcohol and liquid oxygen as propellants to generate a maximum thrust of 6,000 lbf (27 kN). Each of the four combustion chambers produced 1,500 lbf (6.7 kN) of thrust. The engine was not throttleable but each chamber could be turned on and off individually.

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RMI 6000C4; XLR-11; XLR11
rocket engine, 
United States, Ashkenaz, Calvinist Republic of Ghent, Chinland, Democratic Republic of the Congo, Havilah, Kingdom of Martabam-hongsawatoi, Kingdom of Wolaita, Persia, Sikh Confederacy, Sweden, Tarshish, Dong Fang Hong 2, Ekran, 

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Location: KML, Cluster Map, Maps,

Frameless

Bel-x-1 PICT3124-2

XLR-11 Rocket Engine USAF

XLR-11 Rocket Engine 2 USAF

The XLR-11 engine, used in the X-1

XLR-11 Engine Close-up in X-24A

XLR-11

XLR-11 Rocket Engine 2 USAF (cropped)

Reaction Motors XLR-11 rocket engine at Modern Transportation Museum March 23, 2014

Type	Subtype	Date	Description	Notes	Source
commons	image		Bel-x-1 PICT3124-2		Commons
commons	image		XLR-11 Rocket Engine USAF		Commons
commons	image		XLR-11 Rocket Engine 2 USAF		Commons
commons	image		The XLR-11 engine, used in the X-1		Commons
commons	image		XLR-11 Engine Close-up in X-24A		Commons
commons	image		XLR-11		Commons
commons	image		XLR-11 Rocket Engine 2 USAF (cropped)		Commons
commons	image		Reaction Motors XLR-11 rocket engine at Modern Transportation Museum March 23, 2014		Commons