Tupolev ANT-8

Source: Wikipedia, the free encyclopedia.
ANT-8
Role Maritime patrol aircraft
Manufacturer Tupolev
First flight 30 January 1931
Status Retired
Primary user Tupolev Factory
Number built 1

The ANT-8 was an experimental flying boat designed by Tupolev. It was designated the "MDR-2" (MDR meaning Morskoi Dalnii Razvedchik, or Naval Long-Range Reconnaissance) by the military.

Design and development

Tupolev and the

TsAGI were asked to build the ANT-8 in 1925, but other projects were deemed more important. Thus, little was completed on the ANT-8. Finally, in 1930, with Ivan Pogosski leading, actual work was started on the aircraft. Its first flight was on January 30, 1931, piloted by S. Riballschuk. Shortly after the ANT-8 flew for the first time, the ANT-14
lifted off the ground.

Construction

The ANT-8 was chosen to be made entirely from metal, with a

DA-2 machine guns. Up to 500 kg (1,102 lb) of bombs could be carried under the wing roots.[1]

Although the aircraft demonstrated excellent seaworthiness, and Tupolev learned much about flying boat hulls from it, continuation of the ANT-8 project was deemed unnecessary by the

Chetverikov MDR-3
. Only one was built, although its hull was modified several times.

Operators

 Soviet Union

Specifications (MDR-2)

Data from The Osprey Encyclopedia of Russian Aircraft 1875–1995 [2]

General characteristics

  • Crew: 4-5
  • Length: 17.03 m (55 ft 10 in)
  • Wingspan: 23.7 m (77 ft 9 in)
  • Height: 5.67 m (18 ft 7 in) [3]
  • Wing area: 84 m2 (900 sq ft)
  • Airfoil: root:Tupolev A0 (20%) ; tip: Tupolev A0 (14%)[4]
  • Empty weight: 4,560 kg (10,053 lb)
  • Gross weight: 6,920 kg (15,256 lb)
  • Max takeoff weight: 8,160 kg (17,990 lb) [3]
  • Powerplant: 2 × BMW VI V-12 water-cooled piston engines, 507 kW (680 hp) each
  • Propellers: 2-bladed fixed-pitch propellers

Performance

  • Maximum speed: 203 km/h (126 mph, 110 kn)
  • Cruise speed: 166 km/h (103 mph, 90 kn)
  • Range: 1,062 km (660 mi, 573 nmi)
  • Endurance: 5 hours
  • Service ceiling: 3,350 m (11,000 ft)
  • Time to altitude: 1,000 m (3,300 ft) in 7 minutes
  • Power/mass: 0.066 kW/kg (0.040 hp/lb)

Armament

  • Guns: 4 × DA-2 machine guns in nose and dorsal turrets
  • Bombs: Up to 500 kg (1,102 lb) bombs

References

  1. ^ Gunston 1995, p.389.
  2. ^ Gunston 1995, p.390.
  3. ^ a b Duffy and Kandalov 1996, p.208.
  4. ^ Lednicer, David. "The Incomplete Guide to Airfoil Usage". m-selig.ae.illinois.edu. Retrieved 16 April 2019.

Bibliography

  • Duffy, Paul and Andrei Kandalov. (1996) Tupolev, The Man and His Aircraft. Warrendale, PA: Society of Automotive Engineers.
  • Gunston, Bill. The Osprey Encyclopedia of Russian Aircraft 1975–1995. London: Osprey, 1995. .