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Avro Arrow

6,192 recker422  6.6 years ago

The Arrow was the culmination of a series of design studies begun in 1953 examining improved versions of the Avro Canada CF-100 Canuck. After considerable study, the RCAF selected a dramatically more powerful design, and serious development began in March 1955. The aircraft was intended to be built directly from the production line, skipping the traditional hand-built prototype phase. The first Arrow Mk. I, RL-201, was rolled out to the public on 4 October 1957, the same day as the launch of Sputnik I.Flight testing began with RL-201 on 25 March 1958, and the design quickly demonstrated excellent handling and overall performance, reaching Mach 1.9 in level flight. Powered by the Pratt & Whitney J75, another three Mk. 1s were completed, RL-202 through -204. The lighter and more powerful Orenda Iroquois engine was soon ready for testing, and the first Mk.II with the Iroquois, RL-206, was ready for taxi testing in preparation for flight and acceptance tests by RCAF pilots by early 1959. On 20 February 1959, the development of the Arrow (and its Iroquois engines) was abruptly halted before a planned project review had taken place. Two months later, the assembly line, tooling, plans and existing airframes and engines were ordered to be destroyed. The cancellation was the topic of considerable political controversy at the time, and the subsequent destruction of the aircraft in production remains a topic for debate among historians and industry pundits. "This action effectively put Avro out of business and its highly skilled engineering and production personnel scattered. From:R422 P.S this thing was semi torture to build since I haven't built a proper airplane in how many months but I recently was fascinated by this aircraft and decided to put about 2 weeks work into it

General Characteristics

  • Created On iOS
  • Wingspan 35.8ft (10.9m)
  • Length 57.4ft (17.5m)
  • Height 17.4ft (5.3m)
  • Empty Weight 16,011lbs (7,262kg)
  • Loaded Weight 25,358lbs (11,502kg)

Performance

  • Power/Weight Ratio 2.658
  • Wing Loading 44.6lbs/ft2 (217.9kg/m2)
  • Wing Area 568.3ft2 (52.8m2)
  • Drag Points 5286

Parts

  • Number of Parts 97
  • Control Surfaces 5
  • Performance Cost 607