Nikita NB-160 Durva: Difference between revisions
Jump to navigation
Jump to search
No edit summary |
|||
| Line 52: | Line 52: | ||
Powerplant | Powerplant | ||
--> | --> | ||
|eng1 number= | |eng1 number=4 | ||
|eng1 name= | |eng1 name=Kamala TU-1710 | ||
|eng1 type=V-12 inverted liquid-cooled piston engines | |eng1 type=V-12 inverted liquid-cooled piston engines | ||
|eng1 kw=<!-- prop engines --> | |eng1 kw=<!-- prop engines --> | ||
| Line 60: | Line 60: | ||
|eng1 kn=<!-- jet/rocket engines --> | |eng1 kn=<!-- jet/rocket engines --> | ||
|eng1 lbf=<!-- jet/rocket engines --> | |eng1 lbf=<!-- jet/rocket engines --> | ||
|eng1 note={{cvt| | |eng1 note={{cvt|1115|PS|kW hp|0}} | ||
|prop blade number= | |prop blade number=4 | ||
|prop name= | |prop name=constant-speed propellers | ||
|prop dia m=<!-- propeller aircraft --> | |prop dia m=<!-- propeller aircraft --> | ||
|prop dia note= | |prop dia note=5.5 | ||
<!-- | <!-- | ||
Performance | Performance | ||
--> | --> | ||
|max speed kmh= | |max speed kmh=402 | ||
|max speed note=at {{cvt|7000|m|0}} | |max speed note=at {{cvt|7000|m|0}} | ||
|cruise speed kmh= | |cruise speed kmh=322 | ||
|cruise speed note= | |cruise speed note= | ||
|stall speed kmh=105 | |stall speed kmh=105 | ||
| Line 79: | Line 79: | ||
|minimum control speed kmh= | |minimum control speed kmh= | ||
|minimum control speed note= | |minimum control speed note= | ||
|range km= | |range km=8047 | ||
|range note= | |range note= | ||
|combat range km= | |combat range km= 4828 | ||
|combat range note= | |combat range note= | ||
|ferry range km= | |ferry range km= | ||
|ferry range note= | |ferry range note= | ||
|endurance=<!-- if range unknown --> | |endurance=<!-- if range unknown --> | ||
|ceiling m= | |ceiling m=7315 | ||
|ceiling note= | |ceiling note= | ||
|g limits=<!-- aerobatic --> | |g limits=<!-- aerobatic --> | ||
|roll rate=<!-- aerobatic --> | |roll rate=<!-- aerobatic --> | ||
|climb rate ms= | |climb rate ms=24 | ||
|climb rate note= | |climb rate note= | ||
|time to altitude={{cvt|6000|m|0}} in 5 minutes 12 seconds | |time to altitude={{cvt|6000|m|0}} in 5 minutes 12 seconds | ||
Revision as of 21:18, 23 February 2021
| Nikita NB-160 Durva | |
|---|---|
| |
| Role | Heavy Bomber |
| National origin | Tennai |
| Manufacturer | Nikita Aircraft |
| Designer | Kapishan Mishaani |
| First flight | February 1934 |
| Introduction | July 1935 |
| Retired | 1955 |
| Status | Retired |
| Primary user | Royal Tennaiite Air Force |
| Produced | 1935-1950 |
The Nikita NB-160 Durva is a four-engined heavy bomber developed in the 1930s for the Royal Tennaiite Air Force.
Specifications (NB-160 A1)
General characteristics
- Crew: 10 ( Pilot, co-pilot, navigator, bombardier/nose gunner, flight engineer/top turret gunner, radio operator, waist gunners (2), ball turret gunner, tail gunner)
- Length: 35 m (114 ft 10 in)
- Wingspan: 43 m (141 ft 1 in)
- Height: 5.5 m (18 ft 1 in)
- Wing area: 161.3 m2 (1,736 sq ft)
- Empty weight: 14,500 kg (31,967 lb)
- Gross weight: 5,000 kg (11,023 lb)
- Max takeoff weight: 47,600 kg (104,940 lb) 42840
- Powerplant: 4 × Kamala TU-1710 V-12 inverted liquid-cooled piston engines 1,115 PS (820 kW; 1,100 hp)
- Propellers: 4-bladed constant-speed propellers
Performance
- Maximum speed: 402 km/h (250 mph; 217 kn) at 7,000 m (22,966 ft)
- Cruise speed: 322 km/h (200 mph; 174 kn)
- Stall speed: 105 km/h (65 mph; 57 kn)
- Range: 8,047 km (5,000 mi; 4,345 nmi)
- Combat range: 4,828 km (3,000 mi; 2,607 nmi)
- Service ceiling: 7,315 m (23,999 ft)
- Rate of climb: 24 m/s (4,700 ft/min)
- Time to altitude: 6,000 m (19,685 ft) in 5 minutes 12 seconds
Armament
- Guns:
- 4 × 12.72 mm (0.501 in) Basu HV 82 machine guns in fuselage sides
- 2 × 20 mm (0.787 in) Basu FG 20-20 cannon in lower fuselage
- 4× M10 three-tube 4.5 in (112 mm) Hornet 7 rocket launchers; or:
- Inner hardpoints:
- 2× 2,000 lb (907 kg) bombs or drop tanks; or
- 2× 1,000 lb (454 kg) bombs or drop tanks, plus either
- 4× 500 lb (227 kg) bombs or
- 4× 250 lb (113 kg) bombs; or
- 6× 500 lb (227 kg) bombs; or
- 6× 250 lb (113 kg) bombs
- Outer hardpoints:
- 10× 5 in (127 mm) HVARs (High Velocity Aircraft Rockets); or
- 2× 500 lb (227 kg) bombs; or
- 2× 250 lb (113 kg) bombs
- Inner hardpoints: