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CF-105 Arrow vs F-104 Starfighter

CF-105 Arrow vs F-104 Starfighter at a glance — top speed 2,103 vs 2,500 km/h, range 483 vs 2,623 km, max takeoff weight 31,120 vs 13,170 kg, built 5 vs 2,578 units.

Avro CF-105 Arrow combat aircraft side profile drawing
🇨🇦 CF-105 Arrow
Specifications
CF-105 Arrow F-104 Starfighter
Origin country 🇨🇦 Canada 🇺🇸 United States
Category Combat Aircraft Combat Aircraft
Manufacturer Avro Lockheed
First flight 25 March 1958 4 March 1954
Year introduced -- 1958
Number produced 5 units 2578 units
Average unit price $3 million $1.4 million
Wing area 113.8 m² 18.2 m²
Wingspan 15.0 m 6.4 m
Height 6.3 m 4.1 m
Length 23.7 m 16.7 m
Maximum speed 2103 km/h 2500 km/h
Operational range 483 km 2,623 km
Service ceiling 16,154 m 15,240 m
Max. takeoff weight 31,120 kg 13,170 kg
Empty weight 22,245 kg 6,350 kg
Total thrust 2 x 10,659 kgf 1 x 7,076 kgf
Performance Radar Chart

Detailed Comparison

The CF-105 Arrow was a large, twin-engine interceptor designed to counter Soviet bombers over Canada's vast territory, while the F-104 Starfighter was a smaller, single-engine point-defense fighter born from the demand for pure speed and climb performance. The Arrow was a technologically ambitious project cancelled before entering service, with only five test aircraft built. In contrast, the Starfighter became a prolific Cold War asset, with over 2,500 units produced and serving in 15 air forces worldwide, evolving from an interceptor to a multi-role fighter-bomber.

Development and Design

The design philosophies behind the two aircraft were fundamentally different. The Arrow was a large delta-wing platform intended for long-range, high-altitude interception, incorporating advanced features for its time such as a rudimentary fly-by-wire system, extensive use of titanium, and a large internal weapons bay. Its development was a high-risk, high-cost national project intended to go directly to production. The Starfighter, conceived by Lockheed's Kelly Johnson, was a minimalist design focused on maximizing performance with existing technology. Its defining features were a small, thin, trapezoidal wing and a long, slender fuselage. This design optimized for supersonic speed and climb rate but presented significant handling challenges, especially at low speeds, which necessitated a boundary layer control system.

Specifications and Performances

The Arrow was a significantly larger and heavier aircraft, with an empty weight of 22,245 kg, over three times that of the Starfighter's 6,350 kg. This size was necessary for its intended role, requiring two powerful Pratt & Whitney J75 engines. While both aircraft were capable of Mach 2, their performance characteristics diverged sharply in other areas. The Starfighter's primary design goal was reflected in its exceptional climb rate of 244.0 m/s, nearly three times the Arrow's 84.0 m/s, making it a superior quick-reaction interceptor. The Arrow's larger delta wing (113.8 m² vs. the F-104's 18.22 m²) and planned Orenda Iroquois engines in the Mk 2 version were intended to provide superior performance at very high altitudes, with a projected service ceiling of over 70,000 ft for later variants.

Deployment and usage

Operational histories starkly divide the two aircraft. The CF-105 Arrow never entered military service. The program was cancelled on February 20, 1959, due to escalating costs and a strategic shift from bomber threats to intercontinental ballistic missiles (ICBMs). The five completed prototypes were destroyed, leaving the aircraft as a subject of historical debate. Conversely, the F-104 Starfighter had a long and widespread service life, beginning in 1958. It was used by the USAF in the Vietnam War and served as a deterrent during the Taiwan Strait and Berlin crises. Its greatest impact was through export, becoming a primary fighter for many NATO allies, including Germany, Italy, and Canada. Its adaptation into the F-104G multi-role fighter-bomber demonstrated its versatility, though its demanding flight characteristics resulted in a high accident rate in some air forces.

Conclusion

The CF-105 Arrow represents a case of immense but unrealized technological potential, a highly specialized solution whose strategic relevance evaporated before it could mature. Its cancellation underscores the risks of high-cost, single-purpose defense projects. The F-104 Starfighter, while flawed, was a successful design due to its focused performance, adaptability, and lower cost. It became a ubiquitous Cold War fighter that fulfilled a variety of roles for numerous nations, demonstrating that a less ambitious but more flexible and affordable platform can have a far greater strategic impact than a technologically superior but operationally non-existent one.

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Frequently Asked Questions

Which is faster, the CF-105 Arrow or F-104 Starfighter?
The F-104 Starfighter is faster with a maximum speed of 2,500 km/h compared to the CF-105 Arrow's 2,103 km/h, a difference of 397 km/h.
Which has longer range, the CF-105 Arrow or F-104 Starfighter?
The F-104 Starfighter has a longer range at 2,623 km compared to the CF-105 Arrow's 483 km.
Which can fly higher, the CF-105 Arrow or F-104 Starfighter?
The CF-105 Arrow has a higher service ceiling at 16,154 meters (52,998 ft) compared to the F-104 Starfighter's 15,240 meters (50,000 ft).
Which is heavier, the CF-105 Arrow or F-104 Starfighter?
The CF-105 Arrow has a higher maximum takeoff weight at 31,120 kg compared to the F-104 Starfighter's 13,170 kg.
Which is larger, the CF-105 Arrow or F-104 Starfighter?
The CF-105 Arrow is longer at 23.7 meters compared to the F-104 Starfighter's 16.7 meters.
Which is more expensive, the CF-105 Arrow or F-104 Starfighter?
The CF-105 Arrow is more expensive at approximately $3.0 million per unit compared to the F-104 Starfighter at $1.4 million.
Which has been built in greater numbers, the CF-105 Arrow or F-104 Starfighter?
The F-104 Starfighter has been produced in greater numbers with 2,578 units compared to 5 units of the CF-105 Arrow.