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Tupolev Tb-1The Tupolev TB-1 (Тяжелый бомбардировщик - Tyazholy Bombardirovschik - "heavy bomber") (Development name ANT-4) was a Soviet bomber aircraft, an angular monoplane that served as the backbone of the Soviet bomber force for many years. Two 680hp M-17B engines. 212 where built. Development of 1929. Specifications (TB-1) General characteristics - Crew: six
- Length: 18.00 m (59 ft 0 in)
- Wingspan: 28.70 m (94 ft 2 in)
- Height: m ( ft in)
- Wing area: 120.0 m² (1,291 ft²)
- Empty: 4,520 kg (9,944 lb)
- Loaded: 6,810 kg (14,982 lb)
- Maximum takeoff: kg ( lb)
- Powerplant: 2x M-17 inlines, 507 kW (680 hp) each
Performance - Maximum speed: 207 km/h (168 mph)
- Range: 1,000 km (623 miles)
- Service ceiling: 4,830 m (15,842 ft)
- Rate of climb: 170 m/min (557 ft/min)
- Wing loading: 57 kg/m² (12 lb/ft²)
- Power/Mass: 0.15 kW/kg (0.09 hp/lb)
Armament External links: http://www.aviation.ru/Tu/#ANT-4 Related content Related development: Tupolev TB-3 - Tupolev R-6 - Tupolev G-1 Comparable aircraft: Designation sequence (VVS): TB-1 - TB-2 - TB-3 - TB-4 Designation sequence (Tupolev): ANT-1 - ANT-2 - ANT-3 - ANT-4 - ANT-5 - ANT-6 - ANT-7
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