Injector Head, Rocket Engine, R.H. Goddard, Ca. 1929-1930
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This is an injector head for a liquid fuel rocket static tested by American rocket pioneer Dr. Robert H. Goddard from December 1929 to February 1930 at Fort Devens, Massachusetts. Injectors are used to force in the liquid rocket propellant into the motor's combustion chamber for burning in order to drive the rocket forward. Goddard called it the "Dent-Type Injector" because it had conical dents, or depressions, in the square nickel tubes. It also featured a ceramic coating over its facing to absorb heat during the firing of the motor. As a result of the tests, Goddard concluded that the injector was too weak and discarded this design as unsuitable. No flights were attempted at Fort Devens and only static tests were made.
Thee Daniel and Florence Guggenheim Foundation donated this injector to the Smithsonian in 1950.
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
December 1929 - March 1930
Country of Origin
United States of America
Type
PROPULSION-Components (Engine Parts)
Manufacturer
Dr. Robert H. Goddard Dimensions
Overall: 9 1/2 in. long x 7 in. diameter (24.13 x 17.78cm) Materials
Steel pyramid and steel overall; ceramic, then called Insalute cement, coated over injector holes underneath; probably "flake asbestos" inside the frustrum (pyramid) hollow, according to original Goddard notes, Vol. III, p. IX-20, cited below in Documentation. Inventory Number
A19850184000
Credit Line
Gift of the Daniel & Florence Guggenheim Foundation.
Data Source
National Air and Space Museum
Restrictions & Rights
Usage conditions apply
For more information, visit the Smithsonians Terms of Use.