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Continental YJ69-T-7 Turbojet Engine, Incomplete

Air and Space Museum

Object Details

Manufacturer

Continental Aviation and Engineering (Toledo, Ohio)

Designer

Continental, Inc.

Physical Description

Type: Turbojet
Thrust: 4,114 N (925 lb)
Compressor: Single-stage centrifugal
Combustor: Single annular chamber
Turbine: Single-stage axial
Weight: 165 kg (364 lb)

Summary

Continental negotiated a licensing agreement with French engine company Turbomeca in 1951 for the technical rights and U.S. production and marketing of a family of eight small gas turbine engines. With the J69 military designation, Continental significantly improved the design and upgraded the performance of the original Marbore II. In 1952, following intense Continental marketing, Cessna selected the J69 for its candidate in the U.S. Air Force T-37 jet trainer competition, and for some versions of the Ryan Firebee Remotely Piloted Vehicle (RPV). From 1954 through 1995, more than 6,900 J69s were produced for target and reconnaissance versions of the Firebee. And from 1955 through 1976, Continental manufactured more than 3,000 for the Cessna T-37.
This engine, a model YJ69-T-7 Marbore II, was an early flight test engine for the Air Force Firebee RPV. It is not believed to be a production J69 engine.

Credit Line

Transferred from the U.S. Air Force Museum, Wright-Patterson AFB, Ohio

Date

Circa 1950s

Inventory Number

A19600247000

Restrictions & Rights

Usage conditions apply

Type

PROPULSION-Turbines (Jet)

Materials

Steel
Non Magnetic Metal
Anodized Aluminum
Fabric
Paint
Plastic
Rubber
Adhesive

Dimensions

Length 138 cm (54.4 in.), Diameter 57 cm (22.3 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

Metadata Usage

Not determined

Link to Original Record

http://n2t.net/ark:/65665/nv9f8a6d59d-843f-415d-85ba-8a847dbee584

Record ID

nasm_A19600247000

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