Akula TP-87: Difference between revisions
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|ferry range note= | |ferry range note= | ||
|endurance=<!-- if range unknown --> | |endurance=<!-- if range unknown --> | ||
|ceiling m= | |ceiling m=12855 | ||
|ceiling note= | |ceiling note= | ||
|g limits=<!-- aerobatic --> | |g limits=<!-- aerobatic --> | ||
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|climb rate ms= | |climb rate ms= | ||
|climb rate note= | |climb rate note= | ||
|time to altitude={{cvt| | |time to altitude={{cvt|10000|m|0}} in 14 minutes | ||
|wing loading kg/m2= | |wing loading kg/m2= 216.6 | ||
|wing loading note= | |wing loading note= | ||
|fuel consumption kg/km= | |fuel consumption kg/km= | ||
|power/mass= | |power/mass= {{cvt|0.1923|hp/lb|order=flip}} | ||
|more performance= | |more performance= | ||
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|guns=<br/> | |guns=<br/> | ||
:* | :* 4 × {{cvt|20|mm|3}} [[Basu FG 20-35]] cannons in wings, 200 rounds/gun | ||
:* | :* 2 × {{cvt|250|kg}} bombs | ||
:* 2× {{cvt|200|l|usgal}} [[drop tank]]s | |||
|avionics=[[Kol 89]]Z radio | |avionics=[[Kol 89]]Z radio | ||
}} | }} | ||
Revision as of 05:21, 3 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: 12,855 m (42,175 ft)
- Time to altitude: 10,000 m (32,808 ft) in 14 minutes
- Wing loading: 216.6 kg/m2 (44.4 lb/sq ft)
- Power/mass: 0.3161 kW/kg (0.1923 hp/lb)
Armament
- Guns:
- 4 × 20 mm (0.787 in) Basu FG 20-35 cannons in wings, 200 rounds/gun
- 2 × 250 kg (550 lb) bombs
- 2× 200 l (53 US gal) drop tanks
Avionics
Kol 89Z radio