PIK-3

PIK-3
PIK-3a in Finnish Aviation Museum
Role	Sailplane
National origin	Finland
Manufacturer	Polyteknikkojen Ilmailukerho
Designer	Lars Norrmen and Ilkka Lounama
First flight	1950
Number built	40

The PIK-3 (Polyteknikkojen Ilmailukerho - Finnish institute of technology students flying club) was a sailplane produced in Finland in the 1950s and 60s.^[1] It was designed to be a cheap and easy-to-build aircraft^[2] to equip the country's gliding clubs as their standard single-seat machine.^[3] It was a conventional design for its day, with a high wing and conventional empennage.^[2][3] Construction was of wood throughout, skinned in plywood.^[2][3]

Design work commenced in 1942,^[4] but the prototype did not fly until 1950.^[2][3] Antti Koskinen refined the design for production as the PIK-3A and then further modified the design by replacing the flaps with air brakes, which was designated the PIK-3B.^[2][3][4]

By the end of the 1950s, a third modification of the original design was carried out by Olavi Roininen^[4] as the PIK-3C. This had completely new wings of 15 m (49 ft 3 in) to allow it to compete in the Standard Class.^[2] The prototype flew on 20 May 1958,^[2][3] and the design was then modified for production by Suomen Ilmailuliitto.^[3]

Variants

• PIK-3 - first prototype with wingspan of 13 m (47 ft 8 in)
• PIK-3A Kanttikolmonen - initial production version of PIK-3
• PIK-3B - PIK-3A with air brakes in place of flaps
• PIK-3C Kajava - PIK-3B with new wings of 15 m (49 ft 3 in) span

Specifications (PIK-3c)

Data from ,^[2] The World's Sailplanes:Die Segelflugzeuge der Welt:Les Planeurs du Monde^[5]

General characteristics

• Crew: 1
• Length: 6.6 m (21 ft 8 in) (PIK-3 - 6.5 m (21 ft 4 in))
• Wingspan: 15 m (49 ft 3 in) (PIK-3 - 13 m (42 ft 8 in))
• Mid wingspan: 1 m (3 ft 3 in)
• Height: 1 m (3 ft 3 in)
• Wing area: 13.1 m² (141 sq ft) (PIK-3 - 13 m² (140 sq ft))
• Aspect ratio: 17.1 (PIK-3 - 13)
• Airfoil: Göttingen 549 (PIK-3 - Göttingen 693)
• Empty weight: 165 kg (364 lb) (PIK-3 - 135 kg (298 lb))
• Max takeoff weight: 280 kg (617 lb) (PIK-3 - 240 kg (530 lb))

Performance

• Stall speed: 55 km/h (34 mph; 30 kn)
• Never exceed speed: 235 km/h (146 mph; 127 kn) (PIK-3 - 200 km/h (124.3 mph; 108.0 kn))
• Rough air speed max: 145 km/h (90.1 mph; 78.3 kn) (PIK-3 - 130 km/h (80.8 mph; 70.2 kn))
• Aerotow speed: 140 km/h (87.0 mph; 75.6 kn) (PIK-3 - 130 km/h (80.8 mph; 70.2 kn))
• Winch launch speed: 110 km/h (68.4 mph; 59.4 kn) (PIK-3 - 100 km/h (62.1 mph; 54.0 kn))
• Terminal velocity: with full air-brakes at max all-up weight 200 km/h (124 mph; 108 kn) (PIK-3 - 180 km/h (111.8 mph; 97.2 kn))
• g limits: +5 -2.5 (PIK-3 - +4 -2)
• Rate of sink: 0.61 m/s (120 ft/min) at 65 km/h (40.4 mph; 35.1 kn)) (PIK-3 - 0.76 m/s (149.6 ft/min) at 61 km/h (37.9 mph; 32.9 kn))
• Lift-to-drag: 30:1 at 75 km/h (46.6 mph; 40.5 kn)) (PIK-3 - 25:1 at 72 km/h (44.7 mph; 38.9 kn))
• Wing loading: 21.4 kg/m² (4.4 lb/sq ft) (PIK-3 - 18.5 kg/m² (3.79 lb/sqft)

See also

Aircraft of comparable role, configuration and era

Schleicher Ka-6

• Slingsby Skylark 2

Notes

References

Wikimedia Commons has media related to PIK-3.

• Shenstone, B.S.; K.G. Wilkinson & Peter Brooks (1958). The World's Sailplanes:Die Segelflugzeuge der Welt:Les Planeurs dans Le Monde (in Primarily English with French and German) (1st ed.). Zurich: Organisation Scientifique et Technique Internationale du Vol a Voile (OSTIV) and Schweizer Aero-Revue. pp. 9–13.  Cite uses deprecated parameter |coauthors= (help)
• Hardy, Michael (1982). Gliders and Sailplanes of the World. Shepperton: Ian Allan. 
• Coates, Andrew (1978). Jane's World Sailplanes and Motor Gliders. London: MacDonald and Jane's. 
• "PIK-sarjan lentokoneet". Polyteknikkojen Ilmailukerho website. Retrieved 2009-01-08. 
• Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions.