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General Electric I-16, J31, I

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Engine developed from General Electric I-A (copy of British Whittle). First mass produced U.S. turbojet engine.

Technical Specifications
Rated Output 1,650 lbs thrust at 16,500 r.p.m
Compressor 1 stage Centrifugal
Turbine 1 stage axial
Dry Weight 850 lbs
Commonly Used On P-59A & B


Location: Restoration