Valmet PIK-23 Towmaster

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Valmet PIK-23 Towmaster or Suhinu is a Finnish twin-seated glider towing/primary trainer aircraft built entirely out of composite materials in the early 1980s.

The Finnish technology students aviation club suggested in the 1970s, that a new aircraft should be developed for glider towing. The work focused on the improvement of a previous design, the PIK-19 Muhinu. Later on, the Helsinki University of Technology and Valmet Oy joined the project and the design process started from scratch. The goal was to develop a target/glider tower, which also could be used for basic training. It was given the name "PIK-23 Towmaster".

Only two aircraft were manufactured, one at Valmet and one at the Helsinki University of Technology. The first aircraft, OH-TOW, made its maiden flight on March 22, 1982, flown by Mikko Järvi. The second aircraft, OH-TUG, flew the following year.

Valmet marketed the aircraft intensively, but no orders followed. It was also investigated if the aircraft could be sold in parts, for self-assembly, in order to lower the price. In its intended role as a glider tower, the PIK-23 has been quite successful.

Specifications (PIK-23)

Data from Jane's All The World's Aircraft 1982-83 [1]

General characteristics

Performance

  • Never exceed speed: 281 km/h (151 knots, 174 mph)
  • Maximum speed: 250 km/h (135 knots, 155 mph) at sea level
  • Cruise speed: 220 km/h (119 knots, 137 mph) at 3,660 m (12,000 ft), 65% power
  • Stall speed: 78 km/h (42.5 knots, 48.5 mph) (flaps down)
  • Range: 1,250 km (675 nmi, 777 mi)
  • Endurance: 6 hr 30 min (55% power)
  • Service ceiling: 3,650 m[citation needed] (11,972 ft)
  • Rate of climb: 5.8 m/s (1,142 ft/min)

See also


Related lists

References

Notes
  1. Taylor 1982, p.49.
Bibliography
  • Taylor, John W.R. Jane's All The World's Aircraft 1982-83. London:Jane's Yearbooks, 1982. ISBN 0-7106-0748-2.



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