Mahindra V5K: Difference between revisions
Jump to navigation
Jump to search
Line 36: | Line 36: | ||
--> | --> | ||
|crew=1 | |crew=1 | ||
|length m= | |length m=9.75 | ||
|length note= | |length note= | ||
|span m=11 | |span m=11.63 | ||
|span note= | |span note= | ||
|height m=3.27 | |height m=3.27 | ||
|height note= | |height note= | ||
|wing area sqm= | |wing area sqm=21 | ||
|wing area note= | |wing area note= | ||
|aspect ratio=<!-- sailplanes --> | |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>--> | |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= | |empty weight kg=1,901 | ||
|empty weight note= | |empty weight note= | ||
|gross weight kg= | |gross weight kg=2,449 | ||
|gross weight note= | |gross weight note= | ||
|max takeoff weight kg= | |max takeoff weight kg= | ||
Line 74: | Line 74: | ||
Performance | Performance | ||
--> | --> | ||
|max speed kmh= | |max speed kmh=509 | ||
|max speed note=at {{cvt|7000|m|0}} | |max speed note=at {{cvt|7000|m|0}} | ||
|cruise speed kmh= | |cruise speed kmh= |
Revision as of 04:06, 7 January 2022
Mahindra V5K | |
---|---|
Role | Carrier-based fighter |
National origin | Tennai |
Manufacturer | Mahindra Heavy Industries |
Designer | Duwaraga Tanika |
First flight | February 1935 |
Introduction | December 1935 |
Retired | 1945 |
Status | Retired |
Primary user | Royal Tennaiite Navy |
Produced | 1935-1942 |
Number built | 1,517 |
The Mahindra V5K, was a Tennaiite carrier-based fighter aircraft. It was the world's first low-wing monoplane shipboard fighter to enter service and the predecessor to the famous Mahindra V6K "Pujyam". It entered service shortly after the start of the Siduri War in January of 1935 and was quickly deployed to the Tennaiite carriers RK Tipparavai and RK Karutan.
Design and Development
Operational History
Variants
Operators
Specifications (Mahindra V5K4)
General characteristics
- Crew: 1
- Length: 9.75 m (32 ft 0 in)
- Wingspan: 11.63 m (38 ft 2 in)
- Height: 3.27 m (10 ft 9 in)
- Wing area: 21 m2 (230 sq ft)
- Empty weight: 1,901 kg (4,191 lb)
- Gross weight: 2,449 kg (5,399 lb)
- Powerplant: 1 × Nikita E-5 Twin row, 14-cylinder air cooled radial engine 902 PS (663 kW; 890 hp)
- Propellers: 3-bladed metal constant-speed propellers, 3 m (9 ft 10 in) diameter
Performance
- Maximum speed: 509 km/h (316 mph; 275 kn) at 7,000 m (22,966 ft)
- Range: 1,201 km (746 mi; 648 nmi)
- Combat range: 572 km (355 mi; 309 nmi)
- Ferry range: 2,300 km (1,429 mi; 1,242 nmi)
- Service ceiling: 10,000 m (33,000 ft)
- Time to altitude: 3,000 m (9,843 ft) in 3 minutes 35 seconds
- Wing loading: 93.8 kg/m2 (19.2 lb/sq ft)
Armament
- Guns:
- 4 × 7.93 mm (0.312 in) Shrev 97 machine gun
- Bombs:
2 x 30 kg (66 lb) bombs or 1 x 160-litre (42.27 US gallon drop tank)