Object Details
Designer
Armstrong Siddeley
Manufacturer
Buick Motor Division, General Motors Corporation (Wright Aeronautical Division)
Designer
Wright Aeronautical
Physical Description
Type: Turbojet
Thrust: 32,026 N (7,200 lb) at 8,200 rpm
Compressor: 13-stage axial
Combustor: Single annular chamber
Turbine: 2-stage axial
Weight: 1,224 kg (2,696 lb)
Summary
With Air Force encouragement, Wright Aeronautical entered the aircraft gas turbine business when its President Roy T. Hurley traveled to Britain and obtained manufacturing licenses from Bristol for its Olympus turbojet engine, and Armstrong Siddeley for its Sapphire turbojet that had begun development in 1946. Following additional U.S. development, particularly of the compressor and turbine, Wright military qualified the Sapphire as the J65, with production beginning in 1952 and ending in 1957. Wright and Buick built a total of 10,023 J65 engines that powered aircraft such as the Republic F-84 Thunderstreak and RF-84F Thunderflash, the Martin B-57A and RB-57B Canberra, the North American FJ-3 and FJ-4 Fury, Douglas A4D-1 Skyhawk, Grumman F-11 Tiger, and Chance-Vought Regulus missile.
A total of 3,343 J65-B-3 model engines were built, powering the Republic F-84 and RF-84 jet aircraft. The Buick Motor Division of the General Motors Corporation built this J65-B-3 model artifact.
Credit Line
Transferred from the U.S. Air Force Museum, Wright-Patterson AFB, Ohio
Date
1953
Inventory Number
A19600245000
Restrictions & Rights
Usage conditions apply
Type
PROPULSION-Turbines (Jet)
Dimensions
Length 292 cm (115.0 in.), Diameter 95 cm (37.5 in.)
Country of Origin
United States of America
See more items in
National Air and Space Museum Collection
Data Source
National Air and Space Museum
Link to Original Record
Record ID
nasm_A19600245000