Object Details
Manufacturer
Fairchild Engine and Airplane Corporation
Physical Description
Type: Turbojet
Thrust: 4,448 N (1,000 lb) at 15,780 rpm
Compressor: Single-stage mixed-flow
Combustor: Through-flow annular
Turbine: Single-stage axial
Weight: 167.8 kg (370 lb)
Summary
The Fairchild J44 turbojet was created under rigid limitations of weight, size, and thrust for the Navy missile it was to power. The J44 made its first flight in 1950, powering the Petrel air-to-underwater torpedo-carrying missile, and was later selected to power the Ryan high-speed Firebee target drone.
The J44 (commercial designation FT-101E) was qualified for use in manned aircraft in 1955, becoming the first turbojet in its power and weight class to receive an Approved Type Certificate. It powered the Bell Model 65 VTOL Air Test Vehicle. However, no significant manned aircraft applications were found for the J44.
By the late 1950s, the more fuel efficient Continental J69 took the place of the J44 in the Firebee, and the Petrel missile was also phased out about that time. The last batch of J44 engines and spare parts were manufactured in 1959.
Credit Line
Gift of Virginia Polytechnic Institute
Date
1950
Inventory Number
A19650251000
Restrictions & Rights
Usage conditions apply
Type
PROPULSION-Turbines (Jet)
Materials
Aluminum
Magnesium Alloy
Paint
Steel
Rubber
Copper Alloy
Plastic
Cadmium Plating
Phenolic Resin
Natural Fabric
Lead
Silver Plating
Dimensions
3-D (on stand): 208.3 × 76.2 × 75.6cm, 227.3kg (6 ft. 10 in. × 2 ft. 6 in. × 2 ft. 5 3/4 in., 501lb.)
3-D (without stand): 193 × 61.6 × 55.9cm, 167.8kg (6 ft. 4 in. × 2 ft. 1/4 in. × 1 ft. 10 in., 370lb.)
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_A19650251000