Nikita NB-160 Durva: Difference between revisions
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The Nikita NB-160 Durva is a four-engined heavy bomber developed in the 1930s for the Royal Tennaiite Air Force. | 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)== | |||
{{Aircraft specs | |||
|prime units?=met | |||
<!-- | |||
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 m=35 | |||
|length note= | |||
|span m=43 | |||
|span note= | |||
|height m=5.5 | |||
|height note= | |||
|wing area sqm=161.3 | |||
|wing area note= | |||
|aspect ratio=<!-- sailplanes --> | |||
|airfoil=<!--'''root:''' [[NACA airfoil|NACA ]]; '''tip:''' [[NACA airfoil|NACA ]]<ref name="Selig">{{cite web |last1=Lednicer |first1=David |title=The Incomplete Guide to Airfoil Usage |url=https://m-selig.ae.illinois.edu/ads/aircraft.html |website=m-selig.ae.illinois.edu |accessdate=16 April 2019}}</ref>--> | |||
|empty weight kg=14500 | |||
|empty weight note= | |||
|gross weight kg=5000 | |||
|gross weight note= | |||
|max takeoff weight kg=47600 | |||
|max takeoff weight note=42840 | |||
|fuel capacity= | |||
|more general= | |||
<!-- | |||
Powerplant | |||
--> | |||
|eng1 number=2 | |||
|eng1 name=Devati S-P253-117 Deva | |||
|eng1 type=V-12 inverted liquid-cooled piston engines | |||
|eng1 kw=<!-- prop engines --> | |||
|eng1 hp= | |||
|eng1 shp=<!-- prop engines --> | |||
|eng1 kn=<!-- jet/rocket engines --> | |||
|eng1 lbf=<!-- jet/rocket engines --> | |||
|eng1 note={{cvt|1622|PS|kW hp|0}} | |||
|prop blade number=3 | |||
|prop name=light-alloy constant-speed propellers | |||
|prop dia m=<!-- propeller aircraft --> | |||
|prop dia note= | |||
<!-- | |||
Performance | |||
--> | |||
|max speed kmh=684 | |||
|max speed note=at {{cvt|7000|m|0}} | |||
|cruise speed kmh=501 | |||
|cruise speed note= | |||
|stall speed kmh=105 | |||
|stall speed note= | |||
|never exceed speed kmh= | |||
|never exceed speed note= | |||
|minimum control speed kmh= | |||
|minimum control speed note= | |||
|range km=2288 | |||
|range note= | |||
|combat range km= 1144 | |||
|combat range note= | |||
|ferry range km= 3988 | |||
|ferry range note= | |||
|endurance=<!-- if range unknown --> | |||
|ceiling m=13000 | |||
|ceiling note= | |||
|g limits=<!-- aerobatic --> | |||
|roll rate=<!-- aerobatic --> | |||
|climb rate ms=25 | |||
|climb rate note= | |||
|time to altitude={{cvt|6000|m|0}} in 5 minutes 12 seconds | |||
|wing loading kg/m2= | |||
|wing loading note= | |||
|fuel consumption kg/km= | |||
|power/mass= | |||
|more performance= | |||
<!-- | |||
Armament | |||
--> | |||
|guns=<br/> | |||
:* 4 × {{cvt|12.72|mm|3}} [[Basu HV 82]] machine guns in fuselage sides | |||
:* 2 × {{cvt|20|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''': | |||
** Inner hardpoints: | |||
*** 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 08:29, 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: 2 × Devati S-P253-117 Deva V-12 inverted liquid-cooled piston engines 1,622 PS (1,193 kW; 1,600 hp)
- Propellers: 3-bladed light-alloy constant-speed propellers
Performance
- Maximum speed: 684 km/h (425 mph; 369 kn) at 7,000 m (22,966 ft)
- Cruise speed: 501 km/h (311 mph; 271 kn)
- Stall speed: 105 km/h (65 mph; 57 kn)
- Range: 2,288 km (1,422 mi; 1,235 nmi)
- Combat range: 1,144 km (711 mi; 618 nmi)
- Ferry range: 3,988 km (2,478 mi; 2,153 nmi)
- Service ceiling: 13,000 m (43,000 ft)
- Rate of climb: 25 m/s (4,900 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: