CF-100
| CF-100 Canuck | |
|---|---|
 |
|
| No. 423 Squadron Mk 4B CF-100s, 1962. This squadron was based in Grostenquin, France | |
| Role | Interceptor |
| Manufacturer | Avro Canada |
| Designer | John Frost |
| First flight | 19 January 1950 |
| Introduction | 1952 |
| Retired | 1981 |
| Primary users |
Royal Canadian Air Force Belgian Air Force |
| Number built | 692 |
| Variants | Avro Canada CF-103 |
The Avro Canada CF-100 Canuck (affectionately known as the "Clunk") was a Canadian jet interceptor/fighter serving during the Cold War both in NATO bases in Europe and as part of NORAD. The CF-100 was the only Canadian-designed fighter to enter mass production, serving primarily with the Royal Canadian Air Force and Canadian Armed Forces and also in small numbers in Belgium. For its day, the CF-100 featured a short takeoff run and high climb rate, making it well suited to its role as an interceptor.
In the early 1950s, Canada needed an all-weather interceptor (fighter) able to patrol the vast areas of Canada's north and operate in all weather conditions. The two-seat fighter crewed by a pilot and navigator was designed with two powerful engines and an advanced radar and fire control system housed in its nose that enabled it to fly in all-weather or night conditions.
Design of the XC-100 to meet a Royal Canadian Air Force (RCAF) specification for an all-weather fighter was initiated at Avro Canada in October 1946. Chief Engineer Edgar Atkin's work on the CF-100 was subsequently passed to John Frost (formerly of de Havilland) who, along with Avro's Chief Aerodynamacist Jim Chamberlin, reworked the original fuselage design. The CF-100 Mark 1 prototype, "18101," emerged from the factory, painted gloss black overall with white lightning bolts running down the fuselage and engines. The CF-100 prototype flew its maiden flight on 19 January 1950 with Gloster Aircraft Company Chief Test Pilot Squadron Leader Bill Waterton (on loan from Gloster, then also part of the Hawker Siddeley group) at the controls. The Mark 1 was powered by two Rolls-Royce Avon RA 3 turbojets with 28.9 kN (2,950 kgp / 6,500 lbf) thrust each.
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