Object Details
Manufacturer
Rolls-Royce Ltd. (Derby, U.K.)
Physical Description
Type: Turbojet
Thrust: 44,480 N (10,000 lb) at 8,000 rpm
Compressor: 15-stage compound, 6-stage low pressure and 9-stage high pressure axial
Combustor: Cannular
Turbine: 2-stage axial
Weight: 1,709 kg (3,768 lb) (Approximate)
Summary
In 1945, Rolls-Royce started the development of the AJ.65 (axial jet, 28,912 N (6,500 lb) thrust) Avon to replace the Nene, going through several design and test iterations. The first 100-series (RA.3) production engines were delivered in June 1950. For the Comet and Caravelle, the civil RA.29 was produced at 45,592 N (10,250 lb) thrust. The RB.146 300-series was later produced at 76,105 N (17,110 lb) thrust with afterburning.
The Avon powered a variety of military and commercial aircraft: English Electric Canberra, Hawker Hunter, and Vickers-Armstrong Valiant, de Havilland Comet and S.N.C.A.S.E. Caravelle.
This engine, a 44,480 N (10,000 lb) thrust RA.28-49, was manufactured in June 1955 specifically for the Ryan Aeronautical Company in San Diego, California. It powered the Ryan X-13 VTOL Vertijet between 1955 and 1957. In November 1956, the Vertijet, now in the museum's collection, was the first jet-powered VTOL aircraft to demonstrate transition from horizontal to vertical flight and return to horizontal flight.
Credit Line
Transferred from the U.S. Air Force via the contractor, Ryan Aeronautical Company
Date
1955
Inventory Number
A19670027000
Restrictions & Rights
Usage conditions apply
Type
PROPULSION-Turbines (Jet)
Materials
Steel, Aluminum, Magnesium, Preservative coating, Stainless Steel, Inconel, Rubber, Paint
Dimensions
Length 287.8 cm (113.3 in.), Diameter 105.4 cm (41.5 in.)
Country of Origin
United Kingdom
See more items in
National Air and Space Museum Collection
Data Source
National Air and Space Museum
Link to Original Record
Record ID
nasm_A19670027000