General Electric J31-GE-6 (I16-GE-6) Turbojet Engine
Early flight tests of the first General Electric turbojet engine, the Type I-A, clearly showed the need for more powerful engines. GE followed with designs generating increased thrust, including the I-16, designated J31 by the military, which first ran in April 1943. About 250 were built, mainly for variants of the Bell P-59 Airacomet.
When the government believed that future tactical needs would require turbojet engines to use the same fuel as reciprocating engines, GE further developed the engine for the U.S. Navy as a 100-octane, gasoline-burning version of the standard J31 engine, which normally ran on kerosene fuel. That version, along with a Wright R-1820 piston engine, powered the Ryan FR-1 Fireball, the Navy's first partially jet-powered aircraft.
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
Circa World War II
Country of Origin
United States of America
Type
PROPULSION-Turbines (Jet)
Manufacturer
General Electric Aircraft Engines
Physical Description
Type: Turbojet
Thrust: 7,161 N (1,610 lb) at 16,500rpm
Compressor: Single-stage centrifugal
Combustor: 10 reverse-flow chambers
Turbine: Single-stage axial
Weight: 386 kg (850 lb)
Dimensions
3-D: 182.9 × 102.9 × 101.6cm, 385.6kg (6 ft. × 3 ft. 4 1/2 in. × 3 ft. 4 in., 850lb.)
Materials
HAZ MAT: Cadmium
Possible HAZ MAT: Asbestos
Aluminum Alloy
Ferrous Alloy (Steel Most Likely)
Paint
Unidentified Coating
Adhesive Tape
Paper
Adhesive
Inventory Number
A19790120000
Credit Line
Found in collection
Data Source
National Air and Space Museum
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