Chyetverikov MDR-3
MDR-3 | |
---|---|
Role | Arctic Transport Flying Boat |
National origin | USSR |
Manufacturer | Chyetverikov |
Designer | Igor Vyacheslavovich Chyetverikov |
First flight | Template:Avyear |
Number built | 2 |
Variants | Tupolev ANT-27, Tupolev MDR-4, Tupolev MTB-1 |
The MDR-3 (a.k.a.11) was a long-range flying boat designed and built in the USSR from Template:Avyear.
Development
In 1931, Chyetverikov was commissioned to design a new long-range flying boat for MA (Morskaya Aviatsiya – naval aviation), for which Chyetverikov used few new parts, borrowing wings, tailplane and engine nacelles (mounted above the wing) from the Grigorovich TB-5 and a scaled-up Grigorovich ROM-2 fuselage. The use of ready designed or built components led to quick construction of the prototype which was ready for flight tests in Dec 1931, which commenced in January Template:Avyear after the aircraft was transported to Sevastapol in the Crimea. Despite fast construction and excellent structural qualities, results of the flight tests were disappointing, with a takeoff time of 36 seconds, a climb rate of less than a metre per second and a ceiling of only 2,200m, resulting in the whole project being transferred to KOSOS (Konstrooktorskiy Otdel Sektora Opytnovo Stroitel'stva – section of experimental aeroplane construction), due to lack of faith in Chyetverikov's abilities to rectify the poor performance. The MDR-3 became the basis of the ANT-27, MDR-4 and MTB-1.
Specifications (MDR-3)
Data from Gunston, Bill. “The Osprey Encyclopaedia of Russian Aircraft 1875–1995”. London, Osprey. 1995. ISBN 1-85532-405-9
General characteristics
- Crew: six
- Length: 21.9 m (71 ft 10.5 in)
- Wingspan: 32.2 m (105 ft 7.75 in)
- Wing area: 153 m2 (1,649 sq ft)
- Empty weight: 8,928 kg (19,683 lb)
- Gross weight: 13,973 kg (30,805 lb)
- Powerplant: 4 × BMW VI , 507 kW (680 hp) each
Performance
- Maximum speed: 210 km/h (130.5 mph, 113.4 kn)
- Range: 1,600 km (1,000 mi, 870 nmi)
- Service ceiling: 2,200 m (7,218 ft)
- Rate of climb: 4.76 m/s (937.4 ft/min)
Armament
- 1 × machine gun in a nose mounting.
- 1 × machine-gun in a dorsal mounting.
See also
References
- Gunston, Bill. “The Osprey Encyclopaedia of Russian Aircraft 1875–1995”. London, Osprey. 1995. ISBN 1-85532-405-9
- Taylor, Michael J.H. . “ Jane's Encyclopedia of Aviation. Studio Editions. London. 1989. ISBN 0-517-69186-8