To install click the Add extension button. That's it.

The source code for the WIKI 2 extension is being checked by specialists of the Mozilla Foundation, Google, and Apple. You could also do it yourself at any point in time.

4,5
Kelly Slayton
Congratulations on this excellent venture… what a great idea!
Alexander Grigorievskiy
I use WIKI 2 every day and almost forgot how the original Wikipedia looks like.
Live Statistics
English Articles
Improved in 24 Hours
Added in 24 Hours
What we do. Every page goes through several hundred of perfecting techniques; in live mode. Quite the same Wikipedia. Just better.
.
Leo
Newton
Brights
Milds

From Wikipedia, the free encyclopedia

Beriev MDR-5
Role Long-range reconnaissance bombing flying boat
National origin Soviet Union
Manufacturer Beriev
First flight 1938
Primary user Soviet Naval Aviation
Number built 2

The Beriev MDR-5 (Morskoi Dalnii Razvyeedchik - Long-range reconnaissance)(sometimes Beriev MS-5) was a Soviet long-range reconnaissance/bomber flying boat prototype developed by the Beriev design bureau at Taganrog.[1] It did not enter production as the rival Chyetverikov MDR-6 was preferred.

Development

The MDR-5 (Morskoi Dalnyi Razvedchik - naval long-range reconnaissance) was an all-metal twin-engined high-wing cantilever monoplane flying-boat.[1] Designed to be operated by a crew of five it was powered by two Tumansky M-87A radial engines.[1]

Two prototypes were built, the first, a pure flying boat flying which was built in 1938, with the second an amphibian.[2]

Although MDR-5 was adequate, the rival Chyetverikov MDR-6 had already been ordered into production and the MDR-5 was not developed further and remained as prototypes.[3]

Operators

 Soviet Union

Specifications

Data from [1]

General characteristics

  • Crew: 5
  • Length: 15.88 m (52 ft 1 in)
  • Wingspan: 25 m (82 ft 0 in)
  • Wing area: 78.5 m2 (845 sq ft)
  • Empty weight: 6,083 kg (13,411 lb)
  • Max takeoff weight: 8,000 kg (17,637 lb)
  • Powerplant: 2 × Tumansky M-87A radial piston engine, 710 kW (950 hp) each

Performance

  • Maximum speed: 345 km/h (214 mph, 186 kn)
  • Range: 2,415 km (1,501 mi, 1,304 nmi)
  • Service ceiling: 8,150 m (26,740 ft)

Armament

  • Guns: one 7.62mm (0.3in) ShKAS machine-gun in bow and midships manually operated turrets, and one downward firing through a ventral trap
  • Bombs: 1000kg (2204lb)

See also

Related lists

References

Notes

  1. ^ a b c d Orbis 1985, pp. 635-636.
  2. ^ Gunston 1995, p.48.
  3. ^ Nemecek 1986, p.342.

Bibliography

  • Gunston, Bill (1995). The Osprey Encyclopedia of Russian Aircraft from 1875 - 1995. London: Osprey Aerospace. ISBN 1-85532-405-9.
  • Nemecek, Vaclav (1986). The History of Soviet Aircraft from 1918. London: Willow Books. ISBN 0-00-218033-2.
  • The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985). Orbis Publishing.
This page was last edited on 1 June 2023, at 08:24
Basis of this page is in Wikipedia. Text is available under the CC BY-SA 3.0 Unported License. Non-text media are available under their specified licenses. Wikipedia® is a registered trademark of the Wikimedia Foundation, Inc. WIKI 2 is an independent company and has no affiliation with Wikimedia Foundation.