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Canadair CF-104 Starfighter - Canada, 1962


Detailing the development and operational history of the Canadair CF-104 Starfighter Single-Seat Jet-Powered Interceptor / Fighter Aircraft.


 Entry last updated on 6/18/2017; Authored by Staff Writer; Content ¬©www.MilitaryFactory.com

  Canadair CF-104 Starfighter  
Picture of Canadair CF-104 Starfighter


Following the introduction of the American Lockheed F-104 Starfighter came the Canadian equivalent as the CF-104.







Canadair took to producing several American-originated aircraft during the Cold War decades that included the famous Lockheed T-33 "Shooting Star" two-seat trainer (as the CT-133 "Silver Star") and the North American F-86 "Sabre" (as the CF-13 "Sabre"). To replace the latter in the frontline fighter role, it was, again, decided to adopt an American product through local licensed production - this being the Lockheed F-104 "Starfighter". The F-104 became the CF-104 Starfighter in the Royal Canadian Air Force (RCAF) with production out of Canadair of Montreal.

The original F-104 first flew in March of 1954 and was introduced into USAF service during 1958. The Canadair version followed with a first flight on May 26th, 1961 with service entry beginning in March of 1962. Some 200 of the type were built in all and these served until their replacement came during 1983 in the form of the all-modern McDonnell Douglas CF-18 "Hornet", the Canadian version of the American U.S. Navy's F-18 "Hornet" carrier-based fighter line.

Initially, the Canadian fighter replacement program involved a bevy of existing competitors originating from Britain, France, and the United States - the Lockheed F-104G model being one of them. With Lockheed's ongoing relationship with local Canadian aviation industry by way of Canadair and its CT-133 product, the Lockheed submission edged out the competing submissions. The RCAF then contracted Canadair for 200 of the type in August of 1959 with the initial designation being "CF-111" until becoming the more recognizable "CF-104" identifier.






By and large, the Canadian version of the Starfighter differed little from its American F-104G model counterpart. The aircraft first appeared sans the standard 20mm internal cannon to make for more internal fuel volume in the fuselage and, therefore, extend operational ranges of the aircraft. The undercarriage was slightly revised to suit certain RCAF requirements and an inherent reconnaissance and nuclear strike capability was added. The aircraft could carry air-to-air missiles, rocket pods, and conventional drop bombs as needed including nuclear-tipped ordnance options.

The CF-104 was ordered by the RCAF in two distinct production forms - the base CF-104 was the standard single-seat fighter/fighter-bomber variant while the CF-104D followed as a two-seat trainer. D-models retained the performance numbers of their single-seat cousins, seated two in tandem, and were only ever armed with practice munitions. Due to similarities in the Canadair and Lockheed assembly lines, Lockheed was to receive an additional stock of 140 F-104G model aircraft from Montreal beyond the 200 airframes reserved for the RCAF- such were the similarities between the two aircraft.

Externally, the aircraft retained the same design lines of the F-104G models including their tubular, sleek fuselages, short wing mainplanes, and T-style tail unit. The wings were always of considerable interest to onlookers for they were purposely designed as thin with small-an-area as possible so as to reduce drag at high speeds. While this helped the aircraft achieve its amazing performance for the time, it also forced fuel stores to reside within the body of the aircraft alongside avionics, systems, and the like. A single Avro Canada Orenda J79-OEL-7 afterburning turbojet engine powered the type - so a flameout meant that the pilot had no choice to eject and the aircraft was more or less a total loss beyond that. The engine outputted at 10,000lbf on dry thrust and up to 15,800lbf thrust using afterburner.

Once in practice, the aircraft was quickly arranged for the interception role. As a country, the RCAF had to manage a vast airspace locally as well as support ongoing commitments to NORAD and the United States in North America while also continuing its participation with NATO in Europe. The enemy of the day remained the Soviet Union and incursions into North American and European airspace were commonplace throughout the Cold War years. As such, the high, straight line speed and fast rate-of-climb of the CF-104 played well to the strengths of interception - the aircraft could manage speeds reaching 1,145 miles per hour with a 48,000 feet-per-second rate-of-climb. However, the CF-104 initially proved a handful to fly for Canadian airmen as accidents dotting the career of this memorable aircraft with some resulting in deaths during over a quarter century of use by the RCAF. The operating speeds of the aircraft were also a strongpoint along with its relatively contained profile at any approach angle. The 20mm cannon was eventually added back into the CF-104 design when its nuclear-strike role days were behind it.

Operators of CF-104s beyond Canada became Denmark and Norway. The Turkish Air Force received a stock of ex-RCAF aircraft before the end. All RCAF CF-104s were retired and replaced by the CF-18 Hornet line during the 1980s. Turkish use of the CF-104 ended as recently as 1995.




Canadair CF-104 Starfighter Specifications



Service Year: 1962
Type: Single-Seat Jet-Powered Interceptor / Fighter Aircraft
National Origin: Canada
Manufacturer(s): Canadair - Canada
Total Production: 200


Structural (Crew, Dimensions, Weights)



Operating Crew (Typical): 1
Overall Length: 54.79 feet (16.7 meters)
Overall Width: 21.75 feet (6.63 meters)
Overall Height: 13.45 feet (4.10 meters)

Weight (Empty): 13,889 lb (6,300 kg)
Weight (MTOW): 29,035 lb (13,170 kg)

Power / Performance (Engine Type, Top Speed)



Engine: 1 x Avro Canada Orenda J79-OEL-7 turbojet engine with afterburner developing 15,800lbf of thrust.

Maximum Speed: 996 knots (1,146 mph; 1,845 kph)
Maximum Range: 1,420 nautical miles (1,634 miles; 2,630 km)
Service Ceiling: 39,370 feet (12,000 meters; 7.46 miles)
Rate-of-Climb: 48,000 feet-per-minute (14,630 m/min)

Armament / Mission Payload



STANDARD:
1 x 20mm M61A1 Vulcan internal Gatling-style cannon (omitted in early use).

OPTIONAL:
Up to 4,000lbs of stores to include:

AIM-9 Sidewinder short-range air-to-air missiles
Rocket Pods
Conventional Drop Bombs

Global Operators (Customers, Users)



Canada; Denmark; Norway; Turkey

Model Variants



CF-104 - Base series designation; initial production RCAF single-seat fighter/interceptor/fighter-bomber form.
CF-104D - Two-seat trainer for RCAF


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