Akula TP-87: Difference between revisions
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|eng1 number=1 | |eng1 number=1 | ||
|eng1 name= | |eng1 name=Akula AC222 | ||
|eng1 type= | |eng1 type=18-cylinder air-cooled radial piston engine | ||
|eng1 kw= | |eng1 kw=1800 | ||
|eng1 hp= | |eng1 hp= | ||
|eng1 shp=<!-- prop engines --> | |eng1 shp=<!-- prop engines --> | ||
|eng1 kn=<!-- jet/rocket engines --> | |eng1 kn=<!-- jet/rocket engines --> | ||
|eng1 lbf=<!-- jet/rocket engines --> | |eng1 lbf=<!-- jet/rocket engines --> | ||
|eng1 note= | |eng1 note= | ||
|prop blade number= | |prop blade number=4 | ||
|prop name=constant-speed propellers | |prop name=constant-speed propellers | ||
|prop dia m= | |prop dia m= | ||
|prop dia note= | |prop dia note= | ||
<!-- | <!-- | ||
Performance | Performance | ||
--> | --> | ||
|max speed kmh= | |max speed kmh=706 | ||
|max speed note=at {{cvt|6000|m|0}} | |max speed note=at {{cvt|6000|m|0}} | ||
|cruise speed kmh= | |cruise speed kmh=482 | ||
|cruise speed note= | |cruise speed note= | ||
|stall speed kmh= | |stall speed kmh= | ||
Revision as of 16:08, 2 February 2022
| Akula TP-87 | |
|---|---|
| |
| Role | Fighter night fighter |
| National origin | Tennai |
| Manufacturer | Akula Aircraft Company |
| First flight | February 1936 |
| Introduction | August 1936 |
| Retired | 1948 |
| Status | Retired |
| Primary user | Royal Tennaiite Air Force |
| Produced | 1936-1945 |
| Number built | 20,722 |
| Developed into | Cp 218 |
Development
Design
Operational history
Variants
Operators
Specifications (TP-87A-2)
General characteristics
- Crew: 1
- Length: 11.82 m (38 ft 9 in)
- Wingspan: 13.423 m (44 ft 0 in)
- Height: 4.503 m (14 ft 9 in)
- Wing area: 26 m2 (280 sq ft)
- Empty weight: 4,387 kg (9,672 lb)
- Gross weight: 5,632 kg (12,416 lb)
- Max takeoff weight: 6,100 kg (13,448 lb)
- Powerplant: 1 × Akula AC222 18-cylinder air-cooled radial piston engine, 1,800 kW (2,400 hp)
- Propellers: 4-bladed constant-speed propellers
Performance
- Maximum speed: 706 km/h (439 mph; 381 kn) at 6,000 m (19,685 ft)
- Cruise speed: 482 km/h (300 mph; 260 kn)
- Range: 2,020 km (1,255 mi; 1,091 nmi)
- Combat range: 1,010 km (628 mi; 545 nmi)
- Service ceiling: 11,000 m (36,000 ft)
- Time to altitude: 6,000 m (19,685 ft) in 7.8 minutes
Armament
- Guns:
- 2 × 7.93 mm (0.312 in) Basu HV 80 machine guns in wings
- 1 x 20 mm (0.787 in) Basu FG 20-20 cannon firing through propeller hub
Avionics
Kol 89Z radio