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Valmet Vihuri

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Top speed
  
432 km/h

Length
  
8.8 m

First flight
  
February 6, 1951

Wingspan
  
10 m

Retired
  
1959

Manufacturer
  
Valmet

Valmet Vihuri httpsuploadwikimediaorgwikipediacommonsthu

Valmet Vihuri (Finnish for Gale) was a Finnish advanced two-seat fighter trainer aircraft, serving in the Finnish Air Force between 1953 and 1959. Only a few airframes have survived, as in the Central Finland Aviation Museum in Finland.

Contents

History

In spite of their economic problems, the aircraft manufacturer Valmet began designing a new aircraft at the beginning of the 1950s, to replace the aging Finnish Air Force (FAF) VL Pyrys. Martti Vainio was the chief designer of the project. Most of the planning was made by the aeronautical engineers L. Hämäläinen and T. Mäntysalo in 1948–49. The Bristol Mercury, then being manufactured under license in Finland for the Bristol Blenheim bomber, was chosen as the engine, since it was readily available. The prototype (VH-1) made its first flight on February 6, 1951, in Tampere, piloted by captain Esko Halme. After successful test flights, the FAF ordered 30 production aircraft, called Valmet Vihuri II, on February 27, 1951. In the autumn of 1954, the Air Force ordered a further 20 aircraft of the developed version Valmet Vihuri III. All the aircraft of the third version were handed over to the Air Force on January 15, 1957.

Valmet built 51 Vihuris in three different models in Kuorevesi and Tampere. The aircraft had the registration codes VH-1 through VH-51.

Operational use

The Vihuri aircraft became the most-used aircraft in FAF service by the mid-1950s. The aircraft was subject to many accidents, and the press raised much concern over this. The safety of the Vihuri even became a matter for the government. In May 1959, the aircraft was permanently grounded after the death of the Finnish prime minister's son in the aircraft type. Attempts were made to sell the aircraft to Tunisia, without success.

After inspection, it became apparent that the type and its design were sound; most of the accidents were due to pilots' often grave violations of flight regulations, and the fact that all airframes were well worn by the end of the 1950s. The other problem was the engines. The engines used, Tampella Mercury, were recycled engines of wartime Bristol Blenheim bombers which were already worn out. The planes were sold for scrap to Moser OY. One airframe, VH-18, survives in the Central Finland Aviation Museum, and the fore fuselage of another, VH-25, is being restored. The canopies of the scrapped aircraft remain today as the roof windows of the Kuusakoski metal-recycling plant in Espoo.

Operators

 Finland
  • Finnish Air Force
  • Specifications (Valmet Vihuri II)

    Data from Jane's All The World's Aircraft 1956–57

    General characteristics

  • Crew: two
  • Length: 8.80 m (28 ft 9 in)
  • Wingspan: 10.4 m (34 ft 1 in)
  • Height: 3.86 m (12 ft 8 in)
  • Wing area: 18.86 m² (203 sq ft)
  • Empty weight: 2,174 kg (4,793 lb)
  • Loaded weight: 2,678 kg (5,892 lb)
  • Max. takeoff weight: 2,884 kg (6,345 lb)
  • Powerplant: 1 × Bristol Mercury VIII 9-cylinder air-cooled radial, 612 kW (820 hp)
  • Performance

  • Maximum speed: 432 km/h (233 knots, 268 mph) at 3,700 m (12,100 ft)
  • Cruise speed: 327 km/h (177 knots, 203 mph) at 1,000 m (3,300 ft)
  • Range: 665 km (413 mi)
  • Endurance: 2.5 hours
  • Service ceiling: 8,900 m (29,190 ft)
  • Rate of climb: 11.5 m/s (2,263 ft/min)
  • Armament

  • Guns: 2× 7.7 mm Browning machine guns
  • Bombs: 4× 25 kg bombs
  • Preserved aircraft

    The Central Finland Aviation museum is displaying the VH-18, which is the only preserved Vihuri. It gathered 802 flying hours, after which the aircraft served as an educational machine at the Air Force Academy in Kauhava.

    References

    Valmet Vihuri Wikipedia