Valmet Vihuri

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Valmet Vihuri vas a Finnish advanced two-seat fighter trainer aircraft, serving in the Finnish Air Force between 1953 and 1959.

Contents 1 History 2 Operational use 3 Specifications (Valmet Vihuri III) 4 Preserved aircraft 5 Source 6 External links

[edit] History

In spite of their economical problems, the aircraft manufacturer Valmet (began designing a new aircraft in the beginning of the 1950s, to replace the aging FAF VL Pyry's. Martti Vainio was the chief designer of the project. Most of the planning was made by the aeronautic engineers L. Hämäläinen and T. Mäntysalo in 1948–49. The Bristol Mercury was chosen as the engine, since there were no other alternatives. The Mercury was license made in Finland for the Bristol Blenheim bomber. The prototype (VH-1) made its first flight on February 6, 1951 in Tampere, piloted by captain Esko Halme. After the successful test flights, the FAF ordered 30 aircraft of the production series, 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 Vihuri's in three different series (I-III) in Kuorevesi and Tampere. The aircraft had the registration codes VH-1 – VH-51.

[edit] Operational use

The aircraft became the most used aircraft in FAF service by the mid-1950s. The aircraft was subject to many accidents and the press raised a lot of noise about these. The safeness of the Vihure 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.

[edit] Specifications (Valmet Vihuri III)

General characteristics

• Crew: Two
• Length: 8.85 m (29 ft 0 in)
• Wingspan: 10.4 m (34 ft 1 in)
• Height: 3.66 m (12 ft 0 in)
• Wing area: 18.86 m² (203 sq ft)
• Empty weight: 2,174 kg (4,793 lbs)
• Max takeoff weight: 2,704 kg (5,961 lbs)
• Powerplant: 1× Bristol Mercury VIII 9-cyl. air-cooled radial 9-cyl., 626 kW (840 hp)

Performance

• Maximum speed: 444 km/h (276 mph)
• Range: 665 km (413 mi) 2.5 h
• Service ceiling: 8,200 m (26,900 ft)
• Rate of climb: 8.1 m/s (26.6 ft/s)

Armament

• 2× 7,7 mm Browning machine guns
• 4× 25 kg bombs

[edit] 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.

[edit] Source

• Kalevi Keskinen, Kari Stenman, Klaus Niska: Suomen ilmavoimien historia 14 - Suomalaiset hävittäjät, AR-Kustannus ky, 1990. ISBN 951-95821-0-X

[edit] External links

• Pictures from the scrapping of the Vihuris