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Rocket Engine, Liquid Fuel, XLR-11

Display Status:
This object is not on display at the National Air and Space Museum, it is either on loan or in storage.

Rocket Engine, Liquid Fuel, XLR-11

 

  • Summary

Manufacturer:   Reaction Motors, Inc.

Date: ca. 1945-1953

Country of Origin: United States of America

Dimensions:
Overall: 2 ft. wide x 4 ft. 8 1/2 in. long, 210 lb. (60.96 x 143.51cm, 95.3kg)

Materials:
Overall Steel, Adhesive, Synthetic Fabric, Stainless Fabric, Copper, Aluminum, Paint, Stainless Steel, Brass

This is the XLR-11, also called the 6000C-4, one of the most widely used U.S. liquid-propellant rocket engines that powered the Bell X-1 and other rocket research aircraft. Developed by Reaction Motors, Inc. in 1945, it produced a maximum thrust of 6,000 pounds from its four combustion chambers. The engine's most famous application was powering the X-1, the first plane to reach the speed of sound on 14 October 1947.

It was also used in the X-1A, X-1B, X-1D, X-1E, Douglas D-558-1 Skyrocket, and XF-91. Two tandem 6000C-4's served as the Interim Engine for the X-15 from 1960-1961, and it also powered several NASA Lifting Bodies (the HL-10, MS-F3, X-24A, and X-24B). This object was donated to the Smithsonian in 1952 by Reaction Motors, Inc.

Reaction Motors, Inc.


Inventory number: A19530051000