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Rocket Engine, Liquid Fuel, XLR35-RM-1

Air and Space Museum

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International media Interoperability Framework
IIIF provides researchers rich metadata and media viewing options for comparison of works across cultural heritage collections. Visit the IIIF page to learn more.
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Object Details

Manufacturer

Reaction Motors, Inc.

Summary

This is the XLR35-RM-1, the liquid fuel rocket engine that powered the MX-774 test missile, a predecessor of the Atlas intercontinental ballistic missile. The engine produced 8,000 pounds of thrust from four chambers and was also gimballed. This meant it could be steered by the swivelling of each of the four chambers. The propellants were liquid oxygen and alcohol.
Three successful flights of the MX-774 were made at White Sands Proving Grounds, New Mexico, in 1948. No further flights were made, but the engine demonstrated the effectiveness of gimballing and also proved the missile's monocoque airframe, both features later incorporated into the Atlas. This object was donated to the Smithsonian by the Reaction Motors Division of the Thiokol Chemical Corporation in 1985.

Credit Line

Reaction Motors Division, Thiokol Chemical Corp.

Inventory Number

A19850114000

Restrictions & Rights

Usage conditions apply

Type

PROPULSION-Components (Engine Parts)

Materials

Aluminum, Steel, Plastic, Paint, Brass

Dimensions

Overall: 1ft 11 1/2in. x 2ft 2 1/4in., 280lb. (59.69 x 66.68cm, 127kg)
Storage: 138.4 × 82.6 × 112.4cm, 186.9kg (54 1/2 × 32 1/2 × 44 1/4 in., 412lb.)

Country of Origin

United States of America

See more items in

National Air and Space Museum Collection

Data Source

National Air and Space Museum

Metadata Usage

Not determined

Link to Original Record

http://n2t.net/ark:/65665/nv96fc7b2a2-fdeb-451b-a375-20e40a1b9f15

Record ID

nasm_A19850114000

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Rockets and Missiles

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