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Beriev A-40 Albatros

The Beriev A-40 Albatros is a Soviet/Russian jet engine amphibious aircraft designed for the anti-submarine warfare role.

Intended as a replacement for the Beriev Be-12 amphibian and the land-based Ilyushin Il-38, the project was suspended after only one prototype had been manufactured, with the second one 70% completed, due to the breakup of the Soviet Union.

The project was later revived as the A-42 and an order has been placed by the Russian Navy.

The A-40 is a jet-engined flying boat patrol bomber of all-metal construction with the engines located above the wing roots, atop each of the main landing gear nacelles at the rear of each wing root.

The swept wings had a marked anhedral angle, with balance floats attached by short pylons directly under each wingtip.

Variants

A-40

Initial ASW amphibian

1 prototype

A-40M

Projected upgrade to the initial version, utilising a new search and targeting system.

A-40P

Initially a projected aerial firefighting version, able to scoop 25 tonnes (28 tons) of water and transport a team of firefighters.

Later the same designation was used for a projected maritime patrol aircraft in direct competition with the Tupolev Tu-204P.

A-40PM/Be-40P

A projected civil version developed in 1994.

Intended to carry 105 passengers, an export version with CFM engines was also offered.

These studies led to the development of the Beriev Be-200.

Be-40PT

A projected cargo/passenger version designed to carry 70 passengers, 10 tonnes (11 tons) of cargo or 37 passengers and up to 6.5 tonnes of cargo.

A-42/Be-42

A Search and rescue version designed to replace the Beriev Be-12PS, in response to the K-278 disaster.

Construction of a prototype began but was suspended in 1993.

Studies are currently being made of a joint A-42/44 multi-role version, fitted with Progress D-27 propfans.

A-44

Maritime patrol version designed in tandem with the A-42 before the projects were merged into a multi-role aircraft in 1993.

A-42PE

Projected maritime patrol and SAR version intended for export.

Powered by two Progress D-27 propfans.

Specifications

Crew

8

Length

43.84 m (143 ft 10 in)

Wingspan

41.62 m (136 ft 7 in)

Height

11 m (36 ft 1 in)

Wing area

200 m2 (2,200 sq ft)

Max take-off weight

86,000 kg (189,598 lb)

Powerplant

2 × Soloviev D-30KPV turbofan engines,

117.7 kN (26,500 lbf) thrust each

Powerplant

2 × Rybinsk RD-36-35 turbojet engines,

23 kN (5,200 lbf) thrust each take-off boosters

Performance

Maximum speed

800 km/h (500 mph, 430 kn)

Range

4,100 km (2,500 mi, 2,200 nmi) 

Service ceiling

9,700 m (31,800 ft) 

Rate of climb

30 m/s (5,900 ft/min) 

Take-off runs on land

1,000 m (3,281 ft)

Take-off runs on water

2,000 m (6,562 ft)

Landing distance (ground)

700 m (2,297 ft)

Landing distance (water)

900 m (2,953 ft)

Armament
(A-40P ASW Aircraft, internal bomb bay)

Sonobuoys, depth charges, mines,

+

3 Orlan (Sea Eagle) torpedoes,

Or

6 Korshun (Kite) guided missiles

(A-40P ASW Aircraft, underwing pylons)

Kh-35 Anti-ship missiles

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