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Avro Canada CF-100 Canuck

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CF-100 Canuck
No. 423 Squadron Mk 4B CF-100s, 1962. This squadron was based inGrostenquin,France.
Role Interceptor aircraft
Manufacturer Avro Canada
First flight 19 January 1950
Introduction 1952
Retired 1981
Status Withdrawn from service
Primary users Royal Canadian Air Force
Belgian Air Force
Number built 692[1]
Developed into Avro Canada CF-103

TheAvro Canada CF-100 Canuck(affectionately known as the "Clunk" ) is a Canadiantwinjetinterceptor/fighterdesigned and produced by aircraft manufacturerAvro Canada.It has the distinction of being the only Canadian-designed fighter to entermass production.

Work commenced in October 1946 in response to aRoyal Canadian Air Force(RCAF) specification calling for a newjet-poweredinterceptor/fighter aircraft suitable for long-distance patrol missions and all-weather operations. On 19 January 1950, theCF-100 Mark 1prototype,18101,conducted itsmaiden flight,powered by a pair ofRolls-Royce Avon RA 3turbojetengines. Both pre-production and production series aircraft were powered by the domestically-developedAvro Orendaengine instead. Flight testing proved the CF-100 to possess a relatively short takeoff run and a high climb rate, making it well suited to its role as an interceptor. On 18 December 1952, Squadron LeaderJanusz Żurakowski,the Avro company chief development test pilot, took the CF-100 Mk 4 prototype up toMach 1.10in a dive from 14,000 m (45,000 ft),[2]making the type the first straight-winged jet aircraft to achieve controlledsupersonicflight.[citation needed]

The CF-100 principally served with the Royal Canadian Air Force andCanadian Armed Forces;it was also procured in small numbers byBelgiumto equip theBelgian Air Component.Introduced during 1952 amid theCold War,the CF-100 was typically deployed at bothNATObases inEuropeand inNorth Americaas part ofNorth American Aerospace Defense Command(NORAD). In addition to the type's use by frontlinesquadrons,it was also supplied to operational training units and frequently used for other secondary duties, includingaerial reconnaissanceandelectronic warfareroles. During the early 1950s, theAvro Canada CF-103,an advanced derivative of the CF-100 that adopted aswept wingand was capable oftransonicspeeds, was in development, but was terminated. Further development of these concepts ultimately led to theAvro Canada CF-105 Arrow.

During 1981, all of the remaining RCAF CF-100s were withdrawn from service, having been succeeded in the electronic warfare role by theCC-117 Falcon.

Design and development

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Background

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Amid the final years of theSecond World War,officials in Canada had concluded both that the development of a self-sufficient indigenous military aviation industry would be of considerable national value and that the new field ofjet propulsionheld considerable promise. As early as July 1944, Canada had commenced work on its ownturbojetengine programme, producing the experimentalAvro Canada Chinookpowerplant.[3]During the late 1940s and early 1950s, events such as theKorean WarandSoviet atomic bomb projecthad contributed to the rising international tensions of what would become known as theCold War;the Canadian Government decided to respond by greatly increasing defense expenditure.[4]TheRoyal Canadian Air Force(RCAF) was a major recipient of the expanded budget, reaching 46.6% of overall defense expenditure duringFY1951–1952, some of which is attributable to several major procurement programmes that were conducted.[5]

During this period, the RCAF had a strong interest in acquiring its own fleet of jet-powered combat aircraft. Specifically, the service had identified a need for a newjet-poweredinterceptor/fighter aircraft that would be able to patrol the vast areas of Canada's north and operate in all weather conditions. Envisaged as a two-seat fighter, to be crewed by a pilot and navigator, it would adopt two powerful engines along with a relatively advancedradarset andfire control systemhoused in its nose that would enable the aircraft to be operated in all-weather or night conditions. These requirements were formalized by a RCAF specification that was issued during 1946.[citation needed]According to RCAFAir MarshalWilfred Curtis,there was no existing aircraft that could satisfy the specification, nor was there any suitable aircraft already in development elsewhere, thus it was deemed necessary for Canada to develop such a fighter itself.[6]

CF-100 Prototype 18102
Weapons Practice Unit CF-100 Mk 5 firing rockets at first annual Air Defence Command rocket meet,Cold Lake,September 1957.
CF-100 Mk 5D (18476) former CFB Namao and No. 414 Electronic Warfare (EW) Squadron #100476 painted asNo. 440 Squadron RCAFMk 4B serving in NATO and on display at theAlberta Aviation Museum.

On 3 November 1945, an agreement was struck to develop a prototype jet-powered fighter on behalf of the RCAF; on 13 October 1946, the issuing of government contracts to aircraft manufacturerAvro Canadaenabled the company to commence the associated design work.[7]Out of this effort would emerge theXC-100,a prototype all-weather fighter, which was developed to meet the outstanding specification. Work was initially overseen by Edgar Atkin, Avro Canada's Chief Engineer; a key contributor to the programme was ex-de Havillandaircraft designerJohn Frost,who was appointed chief design engineer for military projects and thus responsible for the CF-100's development.[8]At one stage Frost, along with Avro's Chief AerodynamacistJim Chamberlin,extensively reworked the original design of the fuselage.[citation needed]On 17 May 1949, in response to the programme's progress, an additional agreement was reached to produce ten pre-production fighters along with 30Avro Orendas,an indigenously-developed turbojet engine.[8]

Flight testing

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TheCF-100 Mark 1prototype,18101,emerged from the factory, painted gloss black overall with white lightning bolts running down the fuselage and engines. On 19 January 1950, the CF-100 prototype flew itsmaiden flightwithGloster AircraftCompany Chief Test PilotSquadron LeaderBill Waterton(on loan from Gloster, then also part of theHawker Siddeleygroup) at the controls.[9][8]The Mark 1 was powered by a pair ofRolls-Royce Avon RA 3turbojetengines, each capable of generating a maximum thrust of 28.9 kN (2,950 kgp / 6,500 lbf) thrust. During July 1950, the second prototype,18102,performed its first flight.[8]On 5 April 1951, the second prototype was lost in an accident that killed test pilot Bruce Warren. According to aviation author James Dow, this loss resulted in the programme being placed on indefinite hold and questions raised over Avro Canada's competency.[5]

In response to the loss and issues encountered, Avro Canada dismissed several members of the design team and established a special working group to rectify a major structural design error identified.[5]To address the latter, a straightforward modification was developed that could be easily retrofitted into the pre-production aircraft.[5]While both prototypes had been powered by Avon engines, the subsequent pre-production and production series aircraft used the locally developed Orenda powerplant instead, the first of which flying during June 1951. As a result of delays encountered in the development of the Orenda, its selection unavoidably impacted the CF-100 programme's timetable as well.[8]Dissatisfied with the pace of development,Cabinet MinisterC. D. Howeinformed Avro to suspend work on all other projects and focus its efforts on completing the CF-100.[10]

Five pre-productionMk 2test aircraft (serial numbers18103-18107) were produced, all fitted with Orenda 2 engines; one was fitted with dual controls and designated aMk 2Ttrainer. According to pilotJacqueline Cochran,the Orenda engine responded noticeably smoother than any of the British or American-built jet engines that she had previously flown.[11]Initial teething issues with the pre-production aircraft were soon resolved. The first production version, designatedMk 3,made its first flight during October 1952.[1]The Mk 3 incorporated the APG-33 radar and was armed with eight.50caliberBrowning M3machine guns. TheMk 3CTandMk 3DTwere again dual control versions supplied to operational training units.[citation needed]

During mid-January 1955, a CF-100 arrived atEglin AFB,Florida,for cold-weather tests in the climatic hangar. A seven-man RCAF team, headed by Flight Lieutenant B. D. Darling, which had previously conducted tests atNamao Air Base,Alberta,were part of the climatic detachment ofCentral Experimental and Proving Establishment;testing commenced during the following month.[12]In March 1956, a batch of four CF-100 Canucks were dispatched to Eglin AFB to conduct comparative armament trials, where the type was flown by severalUnited States Air Force(USAF) crews.[13]The operational suitability tests, dubbedProject Banana Belt,were carried out by the 3241st Test Group (Interceptor) of the APGC'sAir Force Operational Test Center,in conjunction with a project team belonging to the RCAF.[14]

Production

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During September 1950, the RCAF placed an initial production order for 124 Mk 3 aircraft, the first of which entering service in 1953.[citation needed]This model was armed with eight.50 caliber machine guns. The definitive rocket-armedMk 4Awas based on the prototype Mk 4 (a modified Mk 3), which first flew on 11 October 1952. The nose housed the much largerAPG-40 radar,while the wings were equipped with wingtip pods, each containing up to 29 Mk 4/Mk 40 "Mighty Mouse"folding-fin aerial rocket,to be used in addition to the guns. During 1954, the last 54 of an order for the Mk 3 were swapped for the more advancedMk 4,the total orders for the Mk 4 rose to 510. TheMk 4Bversion was furnished with more powerful Orenda 11s.[citation needed]

Five versions, ormarks,were produced. The high-altitudeMk 5was the final variant, production of which commenced during 1955.[citation needed]This model featured a 1.06 m (3 ft 6 in)-longer wingtip and enlarged tailplane, along with removal of the machine guns. The proposedMk 6was to have mountedSparrow II missilesand been powered byafterburningOrenda 11IR engines; this was intended to be adopted as an "interim" fighter prior to the introduction of the more advancedAvro Canada CF-105 Arrow,which was then under development.[1]An advanced derivative of the CF-100 was theCF-103,which was equipped with aswept wingand projected to be capable oftransonicspeeds; this was built in mock-up form during 1951, but was considered obsolete even before the CF-100's demonstrated ability to exceed the speed of sound in a dive. On 18 December 1952, Squadron LeaderJanusz Żurakowski,the Avro company chief development test pilot, took the CF-100 Mk 4 prototype toMach 1.0in a dive from 9,100 m (30,000 ft), becoming the first straight-winged jet aircraft to achieve controlled supersonic flight.[15][1]

Operational history

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CF-100 Mk 3 at theCanadian Museum of Flightin July 1988.

Amongst RCAF pilots, the Canuck was affectionately known as the "Clunk",[16]the name has been attributed to the noise produced by the forwardlanding gearduring retraction into its well after takeoff. Another common, less attractive, nickname was the "Lead Sled", a reference to its heavy controls and general lack of maneuverability, a nickname that was shared with a number of other 1950s aircraft.[17]Others included CF-Zero, the Zilch, and the Beast, all references to an aircraft many pilots considered less glamorous than RCAFday fighterslike theCanadair Sabre.[18]

Operationally, many CF-100s functioned under the US–CanadianNorth American Air Defense Command(NORAD), which protected North American airspace fromSovietintruders, particularly the threat posed by nuclear-armedbombers.Additionally, between 1956 and 1962, as part of theNorth Atlantic Treaty Organization(NATO), four CF-100 squadrons were based in Europe with1 Air Division;for some time, the CF-100 was the only NATO fighter that was capable of operating in zero visibility and poor weather conditions.[19]

Around the start of theKorean Warin the early 1950s, theUnited States Air Force(USAF) found itself in urgent need of a jet-propelled, all-weather,interdiction/surveillance aircraft.This urgency was so great that the USAF was willing to consider two foreign designs: the CF-100 and theEnglish Electric Canberra.Following an evaluation, the CF-100 was rejected due to its insufficientrangeandpayloadcapabilities; the rivalEnglish Electricdesign was selected and developed into theMartin B-57 Canberra.[20][21]

At its peak, the CF-100 served with nine RCAF squadrons in the mid-1950s. Four of these squadrons were deployed to Europe under the NIMBLE BAT ferry program, replacing multiple NATO RCAF squadrons equipped withCanadair Sabreday fighters to provide all-weather defense against Soviet intruders. While flown in the North American theatre, the CF-100 would typically retain a natural metal finish; however, those flying overseas were given a British-style disruptivecamouflagescheme: dark sea gray and green on top, light sea gray on the bottom.[22]

During his Avro Canada years, the Chief Development Pilot, S/LŻurakowski,continued to fly as an aerobatic display pilot, with spectacular results, especially at the 1955Farnborough Airshowwhere he displayed the CF-100 in a "falling-leaf." He was acclaimed again as the "Great Żura" by many aviation and industry observers who could not believe a large, all-weather fighter could be put through its paces so spectacularly. His performance has been credited withBelgium's decision to purchase the CF-100 for theBelgian Air Force.[16]Additional efforts were made to sell the Canuck to several other nations, including theUnited States,but no other export customers for the type would be secured. Dow reasoned that the Canuck's poor overseas sales performance caused officials to have little confidence for exporting other aircraft, including the CF-105 Arrow.[16]

During the type's production life, 692 CF-100s of different variants were manufactured, including the 53 aircraft that were delivered to the Belgian Air Force. Although originally designed for only 2,000 flight hours, it was found that the Canuck's airframe could serve for over 20,000 hours before needing to be withdrawn. The Belgian aircraft were either scrapped after storage or written off in crashes. Consequently, though the Canadian CF-100 would be replaced in its front line role by the fasterCF-101 Voodoo,the Canuck continued to serve with 414 Squadron of the Canadian Forces, based atCFB North Bay,Ontario;during its later years, the type was tasked withaerial reconnaissance,training andelectronic warfaremissions. It was finally withdrawn from service during 1981.[citation needed]After the CF-100 was retired, a number of aircraft still remain across Canada (and elsewhere) as static displays.

During the late 1950s, an advanced supersonic interceptor,CF-105 Arrowalong with the sophisticatedOrenda Iroquoisengine, was under development by Avro Canada as an intended successor to the CF-100.[23]However, during 1959, work on the CF-105 was terminated following a controversial decision by the Canadian government.

Variants

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  • CF-100 Mk 1:The first two prototypes.
    • CF-100 Mk 1P:Proposed photo-reconnaissance version. Not built.
  • CF-100 Mk 2:Ten pre-production aircraft.
    • CF-100 Mk 2T:Dual control training version of the CF-100 Mk 2. Two built.
  • CF-100 Mk 3:Two-seat all-weather long-range interceptor fighter aircraft. First production version for theRCAF.Eight.5-inch Browning M3guns (200 rounds per gun) in a forward firing ventral gun pack. 70 built.
    • CF-100 Mk 3A:CF-100 Mk 3 sub-type, powered by two Orenda 2 turbojet engines. 21 built.
    • CF-100 Mk 3B:CF-100 Mk 3 sub-type, powered by two Orenda 8 turbojet engines. 45 built.
    • CF-100 Mk 3CT:One CF-100 Mk 3 converted into a dual control training aircraft. Later redesignatedCF-100 Mk 3D.
  • CF-100 Mk 4:Two-seat all-weather long-range interceptor fighter aircraft. Eight.5-inch Browning M3 guns (200 rounds per gun) in a forward firing ventral gun pack. Plus two wingtip pods of 29 x 70-mm (2.75 in) "Mighty Mouse"fin-folding aerial rockets.One pre-production aircraft.
18241 – CF-100 Mk.4A on static display at theNational Museum of the United States Air ForceatWright-Patterson AFBinDayton, Ohio.
    • CF-100 Mk 4A:CF-100 Mk 4 sub-type, powered by two Orenda 9 turbojet engines. 137 built.
    • CF-100 Mk 4B:CF-100 Mk 4 sub-type, powered by two Orenda 11 turbojet engines. 141 built.
    • CF-100 Mk 4X:Proposed version of the CF-100 Mk 4. Not built.
  • CF-100 Mk 5:Two-seat all-weather long-range interceptor fighter aircraft, powered by two Orenda 11 or Orenda 14 turbojet engines. Two wingtip pods of 29 x 70-mm (2.75 in) "Mighty Mouse" fin-folding aerial rockets. 332 built.
    • CF-100 Mk 5D:Small number of CF-100 Mk 5s converted into ECM (Electronic Countermeasures), EW (Electronic Warfare) aircraft.
    • CF-100 Mk 5M:Small number of CF-100 Mk 5s equipped to carry theAIM-7 SparrowII air-to-air missiles.
  • CF-100 Mk 6:Proposed version armed with theAIM-7 SparrowII air-to-air missile. Not built.

Operators

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CF-100 badge worn by Canadian Forces crews in the 1970s and 80s
Belgium
Canada

Notable accidents and incidents

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  • 11 August 1953: a CF-100 crashed inLongueuil, Québecshortly after take-off, killing both crewmen. Two houses were struck, killing seven on the ground including five children - all six years old and younger.[24]
  • 15 May 1956: A CF-100 crashed into the Villa St. Louis atOrléans, Ontario,killing both crewmen and 13 civilians on the ground in what is known as theConvent Crash.
  • 25 August 1958: Two CF-100s in a four-aircraft formation collided and crashed atNo. 2 (F) Wing, Grostenquin, France.One aircraft crashed into the base hospital and one crashed into a field. Two people were killed in the hospital and three aircrew were killed.[25]

Aircraft on display

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Avro Canada CF-100 Canuck Mk.3D on display at the Nanton Air Museum, Nanton, Alberta.
Canadian Forces CF-100 on display at Head Lake Park, Haliburton, Ontario
RCAF CF-100 at Lee Park, North Bay
CF-100 National Air Force Museum of Canada, Trenton, Ontario

Belgium

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Canada

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United Kingdom

[edit]

United States

[edit]

Specifications (CF-100 Mk 5)

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Data from[citation needed]

General characteristics

  • Crew:two
  • Length:54 ft 2 in (16.51 m)
  • Wingspan:57 ft 2 in (17.42 m)
  • Height:14 ft 6 in (4.42 m)
  • Wing area:591 sq ft (54.9 m2)
  • Empty weight:23,100 lb (10,478 kg)
  • Gross weight:33,450 lb (15,173 kg)
  • Max takeoff weight:36,000 lb (16,329 kg)[65]
  • Powerplant:2 ×Avro Canada Orenda 11turbojetengines, 7,300 lbf (32 kN) thrust each

Performance

  • Maximum speed:552 mph (888 km/h, 480 kn)
  • Range:2,000 mi (3,200 km, 1,700 nmi)
  • Service ceiling:45,000 ft (14,000 m)
  • Rate of climb:8,750 ft/min (44.5 m/s)
  • Thrust/weight:0.44

Armament

  • Rockets:2 wingtip pods of 29 x 70-mm (2.75 in) "Mighty Mouse" fin-folding aerial rockets

Avionics

  • Radar

See also

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Related development

Aircraft of comparable role, configuration, and era

Related lists

References

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Citations

[edit]
  1. ^abcdDow 1997, p. 72.
  2. ^Page 1981, p. 64.
  3. ^Dow 1997, pp. 62-63.
  4. ^Dow 1997, pp. 66-70.
  5. ^abcdDow 1997, p. 70.
  6. ^Dow 1997, pp. 64-65.
  7. ^Dow 1997, p. 63-65.
  8. ^abcdeDow 1997, p. 69.
  9. ^Rossiter 2002, p. 63.
  10. ^Dow 1997, pp. 70-72.
  11. ^Dow 1997, p. 73.
  12. ^"Eglin Will Test New All-Weather RCAF Interceptor".The Okaloosa News-Journal,Crestview, Florida, Volume 41, Number 3, 20 January 1955, p. 6.
  13. ^"ADA-Arrow Pilots: Jan Zurakowski."Avroarrow.org.Retrieved: 31 October 2011.
  14. ^"Eglin Tests Latest Canadian Jet Model".The Okaloosa News-Journal,Crestview, Florida, Volume 42, Number 14, 5 April 1956, p. 20.
  15. ^Whitcomb 2008, p. 89.
  16. ^abcDow 1997, p. 74.
  17. ^"Designation Systems".users.skynet.be.
  18. ^"CF-100 Veterans Reunite."ArchivedJuly 7, 2011, at theWayback MachineComox Valley Echo,18 September 1998. Retrieved: 7 February 2010.
  19. ^Baglow pp 101-113
  20. ^"English Electric Canberra B-57 Prototype."ArchivedJuly 5, 2012, at theWayback MachineNational Museum of the USAF.Retrieved: 7 February 2010.
  21. ^Baugher, Joe."Martin B-57A."USAAC/USAAF/USAF Bomber Aircraft-Third Series,13 August 2006. Retrieved: 7 February 2010.
  22. ^Baglow, pp 101-121
  23. ^Milberry 1984, p 320.
  24. ^Services Simple, Brief and Sad for Five Victims of Air CrashThe Montreal Gazette,15 August 1953 Retrieved: 11 March 2020
  25. ^"Grostenquin, France - 423 Squadron History."c-and-e-museum.org,Retrieved: 30 July 2018.
  26. ^"Airframe Dossier - Avro CanadaCF-100, s/n 18534 CAF, c/n C-100/5/434".Aerial Visuals.AerialVisuals.ca.Retrieved22 July2017.
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  39. ^"Airframe Dossier - Avro Canada CF-100Mk 5 Canuck, s/n 18746 CAF, c/n C-100/5/646".Aerial Visuals.AerialVisuals.ca.Retrieved22 July2017.
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  41. ^"Aviation".Reynolds Museum.Government of Alberta.Retrieved1 December2019.
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  43. ^"Canuck".National Air Force Museum of Canada.National Air Force Museum of Canada.Retrieved21 July2017.
  44. ^"Airframe Dossier - Avro Canada CF-100 Canuck, s/n 18784 RCAF, c/n C-100/5/684".Aerial Visuals.AerialVisuals.ca.Retrieved22 July2017.
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  65. ^Taylor and Alexander 1969, p. 51.

Bibliography

[edit]
  • Baglow, Bob.Canucks Unlimited: Royal Canadian Air Force CF-100 Squadrons and Aircraft, 1952–1963.Ottawa, Ontario, Canada: Canuck Publications 1985.ISBN0-9692246-0-5.
  • Dow, James.The Arrow.James Lorimer & Company, 1997.ISBN1-5502855-4-8.
  • Henley, Don (March–April 1997). "Singular Customer: Belgium and the Avro Canada CF-100".Air Enthusiast.No. 68. pp. 60–63.ISSN0143-5450.
  • Lyzun, Jim.CF-100 Canuck.Ottawa, Ontario, Canada: SMS Publishing, 1985.ISBN0-920375-04-9.
  • Milberry, Larry.The Avro CF-100.Toronto, Ontario, Canada: CANAV Books, 1981.ISBN0-9690703-0-6.
  • Milberry, Larry.Sixty Years, The RCAF and CF Air Command 1924–1984.CANAV Books, 1984.ISBN0-07-549484-1.
  • Page, Ron.Canuck: CF-100 All Weather Fighter.Erin, Ontario, Canada: Boston Mills Press, 1981.ISBN0-919822-39-8.
  • Taylor, John W. R. and Jean Alexander.Combat Aircraft of the World.New York: G.P. Putnam's Sons, 1969.ISBN0-71810-564-8.
  • Whitcomb, Randall L.Cold War Tech War: The Politics of America's Air Defense.Burlington, Ontario, Canada: Apogee Books, 2008.ISBN978-1-894959-77-3.
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