Nikita NB-160 Durva: Difference between revisions

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|guns=<br/>
|guns=<br/>
:* 4 × {{cvt|12.72|mm|3}} [[Basu HV 82]] machine guns in fuselage sides
** 6 × {{cvt|7.62|mm|3}} [[Basu HV 82]] machine guns in fuselage sides
:* 2 × {{cvt|20|mm|3}} [[Basu FG 20-20 cannon]] in lower fuselage
** 4 × {{cvt|12.72|mm|3}} [[Basu FG 20-20 cannon]] in lower fuselage
* 4× M10 three-tube 4.5 in (112 mm) [[Hornet 7 (rocket)|Hornet 7 rocket]] launchers; '''or''':
*'''Bombs'''
** Inner hardpoints:
** Up to {{convert|5520|kg|lb|0|abbr=on}} bombs
*** 2× {{convert|2000|lb|kg|0|abbr=on}} bombs or drop tanks; '''or'''
 
*** 2× {{convert|1000|lb|kg|0|abbr=on}} bombs or drop tanks, plus either
**** 4× {{convert|500|lb|kg|0|abbr=on}} bombs or
**** 4× {{convert|250|lb|kg|0|abbr=on}} bombs; '''or'''
*** 6× {{convert|500|lb|kg|0|abbr=on}} bombs; '''or'''
*** 6× {{convert|250|lb|kg|0|abbr=on}} bombs
** Outer hardpoints:
*** 10× 5 in (127 mm) [[HVAR]]s (High Velocity Aircraft Rockets); '''or'''
*** 2× {{convert|500|lb|kg|0|abbr=on}} bombs; '''or'''
*** 2× {{convert|250|lb|kg|0|abbr=on}} bombs
}}
}}

Revision as of 04:56, 24 February 2021

Nikita NB-160 Durva
Devati 191.jpg
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 was 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:
  • Bombs
    • Up to 5,520 kg (12,170 lb) bombs