This is the regeneratively-cooled liquid fuel rocket motor designed and built in 1942 by James H. Wyld of the American Rocket Society (ARS) for the Navy. It is a copy of the original Wyld motor, built in 1937 and successfully tested in 1938 and 1941.

One major problem facing early rocket experimenters was a suitable cooling for their motors, which often over-heated. In the regenerative system, the propellant circulates around the motor's cooling jacket before injection into the combustion chamber, where it is ignited with the oxidizer (liquid oxygen). Wyld, with three other ARS members, formed Reaction Motors, Inc. (RMI) in 1941 to develop the Wyld engine. RMI thus produced reliable JATO (Jet-Assisted-Take-Off) motors to help lift large, heavily-loaded planes. The motor was donated to the Smithsonian in 1968 by the Aerojet General Corp.

Display Status

This object is not on display at the National Air and Space Museum. It is either on loan or in storage.

Object Details

Date

1942

Country of Origin

United States of America

Type

PROPULSION-Rocket Engines

Manufacturer

James Hart Wyld

Dimensions

3-D: 24.1 × 14 × 8.9cm, 1.8kg (9 1/2 × 5 1/2 × 3 1/2 in., 4lb.)

Materials

Cooling jacket, steel; rods and bolts, steel; retainer rings (two), Chrome-plated steel; propellant inlet,, non-ferrous, Chrome-plated; B-nut, brass; top fixture (ignitor unit), probably brass; nozzle nut, brass; nozzle, proper, non-ferrous

Inventory Number

A19680226000

Credit Line

Gift of Aerojet General Corporation

Data Source

National Air and Space Museum

Restrictions & Rights

Usage conditions apply
For more information, visit the Smithsonians Terms of Use.