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The Bartini Beriev VVA-14 Vertikal`no-Vzletayuschaya Amphibia ( ) was a
developed in the Soviet Union during the 1970s. Designed to be able to take-off from the water and fly at high speed over long distances, it was to make true flights at high altitude, but also have the capability of 'flying' efficiently just above the sea surface, using aerodynamic . The VVA-14 was designed by
in answer to a perceived requirement to destroy
submarines.
Bartini, in collaboration with the
intended to develop the prototype VVA-14 in three phases. The VVA-14M1 was to be an aerodynamics and , initially with rigid pontoons on the ends of the central wing section, and later with these replaced by inflatable pontoons. The VVA-14M2 was to be more advanced, with two starting engines to blast into the cavity under the wing to give lift and later with a battery of lift engines to give VTOL capability, and with . The VVA-14M3 would see the VTOL vehicle fully equipped with armament and with the Burevestnik computerised ASW () system, Bor-1 MAD () and other operational equipment.
After extensive research, including the development of the small prototype
wing in ground effect aircraft, the first VVA-14 prototype was completed in 1972. Its first flight was from a conventional runway on 4 September 1972.
In 1974 the inflatable pontoons were installed, though their operation caused many problems. Flotation and water taxi tests followed, culminating in the start of flight testing of the amphibious aircraft on 11 June 1975.
The inflatable pontoons were later replaced by rigid pontoons, while the fuselage was lengthened and the starting engines added. This incarnation was given the designation 14M1P. However, the bureau supplying the intended battery of 12 RD-36-35PR lift engines did not deliver, and this made VTOL testing impossible.
After Bartini's death in 1974, the project slowed and eventually drew to a close, the aircraft having conducted 107 flights, with a total flight time of 103 hours. The only remaining VVA-14, No. 19172, was retired to the , Monino in 1987. The aircraft still resides at the museum in a dismantled state, where it carries the number '10687' and 'Aeroflot'.
General characteristics
Length: 25.97 m (85 ft 2 in)
Wingspan: 30 m (98 ft 5 in)
Height: 6.79 m (22 ft 3 in)
Wing area: 217.79 m2 (2344 ft2)
Empty weight: 23,236 kg (51,119 lb)
Gross weight: 52,000 kg (114,400 lb)
Powerplant: (Cruise) 2 × D-30M turbofans, 67 kN (15062 lbf) thrust each
(VTOL - not fitted) 12 × 12 RD-36-35 PR lift turbofan engines, 43 kN (9,666 lbf) thrust each
Performance
Maximum speed: 760 km/h (472 mph)
Cruising speed: 640 km/h (398 mph)
Range: 2,450 km (1,522 miles)
Service ceiling: 8,000-10,000 m (26,247-32,808 ft)
Related development
*Komissarov, Sergey. “Russia's Ekranoplans”. Hinkley. Midland Publishing. 2002.
. Archived from
Komissarov, Sergey. “Russia's Ekranoplans”. Hinkley. Midland Publishing. 2002.
Komissarov, Sergey and Yefim Gordon. Soviet and Russian Ekranoplans. Hersham, UK: Ian Allen Publishing, 2010. .
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