The 3,057 kw (4,100 ehp) XT34-P-2 was developed originally as a dependable simple-cycle turboprop engine for use in high performance, long-range aircraft. It was intended that it might later be developed into a free turbine engine. A design contract for the T34-P-2 was issued in 1945, and amended in 1946 to continue development and component testing. The first engine was tested in January 1948.

The T34 turboprop engine first flew in September 1950, installed in the nose of a B-17 flying test bed, and the four-engine Boeing KC-97J, which survived as the B-377 Super Guppy, was its first application. The Air Force then selected the P-3 model for the Douglas C-133A Cargomaster, also having four engines.

Later development resulted in the 6,816 kw (9,140 ehp) XT48-P-2, which was considered for the dual engine VP-HL, a heavy, land based naval patrol aircraft that eventually led to the well known four-engine P-3 Orion.

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 1953 Country of Origin United States of America Type PROPULSION-Turbines (Jet) Manufacturer Pratt & Whitney
Physical Description Type: Turboprop Power rating: 4,474 kW (6,000 ehp) at 11,000 rpm Compressor: 13-stage axial Combustor: 8 through-flow, can-type Turbine: 3-stage axial Weight: 1,211 kg (2,670 lb) Dimensions 3-D: 401.3 × 82.5 × 102.9cm, 1211.1kg (13 ft. 2 in. × 2 ft. 8 1/2 in. × 3 ft. 4 1/2 in., 2670lb.)
Materials HAZ MAT: Asbestos
Ferrous Alloy
Aluminum Alloy
Plastic
Wood
Paint
Grease
Copper Alloy
Inventory Number A19721344000 Credit Line Transferred from the U.S. Air Force, Dover AFB, Delaware Data Source National Air and Space Museum Restrictions & Rights Usage conditions apply
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