Akula TP-87: Difference between revisions
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==Operators== | ==Operators== | ||
*{{flag|Tennai}} | *{{flag|Tennai}} | ||
==Specifications (TP-87A-2)== | |||
{{Aircraft specs | |||
|prime units?=met | |||
<!-- | |||
General characteristics | |||
--> | |||
|crew=1 | |||
|length m=11.82 | |||
|length note= | |||
|span m=13.423 | |||
|span note= | |||
|height m=4.503 | |||
|height note= | |||
|wing area sqm=26 | |||
|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=4387 | |||
|empty weight note= | |||
|gross weight kg=5632 | |||
|gross weight note= | |||
|max takeoff weight kg=6100 | |||
|max takeoff weight note= | |||
|fuel capacity= | |||
|more general= | |||
<!-- | |||
Powerplant | |||
--> | |||
|eng1 number=1 | |||
|eng1 name=Kamala 1710-13 | |||
|eng1 type=V-12 inverted liquid-cooled piston engines | |||
|eng1 kw=<!-- prop engines --> | |||
|eng1 hp=1175 | |||
|eng1 shp=<!-- prop engines --> | |||
|eng1 kn=<!-- jet/rocket engines --> | |||
|eng1 lbf=<!-- jet/rocket engines --> | |||
|eng1 note= | |||
|prop blade number=3 | |||
|prop name=constant-speed propellers | |||
|prop dia m=2.8 | |||
|prop dia note= | |||
<!-- | |||
Performance | |||
--> | |||
|max speed kmh=670 | |||
|max speed note=at {{cvt|6000|m|0}} | |||
|cruise speed kmh=552 | |||
|cruise speed note= | |||
|stall speed kmh= | |||
|stall speed note= | |||
|never exceed speed kmh= | |||
|never exceed speed note= | |||
|minimum control speed kmh= | |||
|minimum control speed note= | |||
|range km=2020 | |||
|range note= | |||
|combat range km= 1010 | |||
|combat range note= | |||
|ferry range km= | |||
|ferry range note= | |||
|endurance=<!-- if range unknown --> | |||
|ceiling m=11000 | |||
|ceiling note= | |||
|g limits=<!-- aerobatic --> | |||
|roll rate=<!-- aerobatic --> | |||
|climb rate ms= | |||
|climb rate note= | |||
|time to altitude={{cvt|6000|m|0}} in 7.8 minutes | |||
|wing loading kg/m2= | |||
|wing loading note= | |||
|fuel consumption kg/km= | |||
|power/mass= | |||
|more performance= | |||
<!-- | |||
Armament | |||
--> | |||
|guns=<br/> | |||
:* 2 × {{cvt|7.93|mm|3}} [[Basu HV 80]] machine guns in wings | |||
:* 1 x {{cvt|20|mm|3}} [[Basu FG 20-20]] cannon firing through propeller hub | |||
|avionics=[[Kol 89]]Z radio | |||
}} | |||
Revision as of 16:02, 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 × Kamala 1710-13 V-12 inverted liquid-cooled piston engines, 876 kW (1,175 hp)
- Propellers: 3-bladed constant-speed propellers, 2.8 m (9 ft 2 in) diameter
Performance
- Maximum speed: 670 km/h (416 mph; 362 kn) at 6,000 m (19,685 ft)
- Cruise speed: 552 km/h (343 mph; 298 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