Cheppali Cp 120: Difference between revisions
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The Cheppali Cp 120 was a Tennaiite Siduri War fighter aircraft design from Cheppali. It served alongside the Cheppali Cp 117 and Nikita N.167. | |||
==Development== | ==Development== | ||
===Design=== | ===Design=== | ||
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Performance | Performance | ||
--> | --> | ||
|max speed kmh= | |max speed kmh=670 | ||
|max speed note=at {{cvt| | |max speed note=at {{cvt|6000|m|0}} | ||
|cruise speed kmh= | |cruise speed kmh=552 | ||
|cruise speed note= | |cruise speed note= | ||
|stall speed kmh= | |stall speed kmh= | ||
|stall speed note= | |stall speed note= | ||
|never exceed speed kmh= | |never exceed speed kmh= | ||
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|minimum control speed kmh= | |minimum control speed kmh= | ||
|minimum control speed note= | |minimum control speed note= | ||
|range km= | |range km=2020 | ||
|range note= | |range note= | ||
|combat range km= | |combat range km= 1010 | ||
|combat range note= | |combat range note= | ||
|ferry range km= | |ferry range km= | ||
|ferry range note= | |ferry range note= | ||
|endurance=<!-- if range unknown --> | |endurance=<!-- if range unknown --> | ||
|ceiling m= | |ceiling m=11000 | ||
|ceiling note= | |ceiling note= | ||
|g limits=<!-- aerobatic --> | |g limits=<!-- aerobatic --> | ||
|roll rate=<!-- aerobatic --> | |roll rate=<!-- aerobatic --> | ||
|climb rate ms= | |climb rate ms= | ||
|climb rate note= | |climb rate note= | ||
|time to altitude={{cvt|6000|m|0}} in | |time to altitude={{cvt|6000|m|0}} in 7.8 minutes | ||
|wing loading kg/m2= | |wing loading kg/m2= | ||
|wing loading note= | |wing loading note= | ||
Revision as of 06:56, 9 March 2021
| Cheppali Cp 120 | |
|---|---|
| |
| Role | Fighter |
| National origin | Tennai |
| Manufacturer | Cheppali |
| Designer | Lathusa Prithiyanga |
| First flight | March 1936 |
| Introduction | February 1937 |
| Retired | 1948 |
| Status | Retired |
| Primary user | Royal Tennaiite Air Force |
| Produced | 1936-1947 |
| Number built | 15,468 |
The Cheppali Cp 120 was a Tennaiite Siduri War fighter aircraft design from Cheppali. It served alongside the Cheppali Cp 117 and Nikita N.167.
Development
Design
Engine collant and oil cooling systems
World speed record
Prototypes
Operational history
Siduri War
Foreign use
Variants
Specifications (Cp 1120 D-1)
General characteristics
- Crew: 1
- Length: 8.2 m (26 ft 11 in)
- Wingspan: 9.4 m (30 ft 10 in)
- Height: 3.60 m (11 ft 10 in)
- Wing area: 14.6 m2 (157 sq ft)
- Empty weight: 1,810 kg (3,990 lb)
- Max takeoff weight: 2,500 kg (5,512 lb)
- Fuel capacity: 300 kg (660 lb)
- Powerplant: 1 × Kamala 1710 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 firing through propeller hub
Avionics
Kol 89Z radio