Mahindra V5K: Difference between revisions
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==Variants== | ==Variants== | ||
==Operators== | ==Operators== | ||
==Specifications ( | ==Specifications (Mahindra V5K4)== | ||
[[File:Mitsubishi A5M.svg|frameless|right|upright=1.35|Orthographically projected diagram of the Cp 117 B2-L2]] | [[File:Mitsubishi A5M.svg|frameless|right|upright=1.35|Orthographically projected diagram of the Cp 117 B2-L2]] | ||
{{Aircraft specs | {{Aircraft specs | ||
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--> | --> | ||
|crew=1 | |crew=1 | ||
|length m= | |length m=7.565 | ||
|length note= | |length note= | ||
|span m=11 | |span m=11 | ||
|span note= | |span note= | ||
|height m=3. | |height m=3.27 | ||
|height note= | |height note= | ||
|wing area sqm= | |wing area sqm=17.8 | ||
|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=1300 | ||
|empty weight note= | |empty weight note= | ||
|gross weight kg= | |gross weight kg=1750 | ||
|gross weight note= | |gross weight note= | ||
|max takeoff weight kg= | |max takeoff weight kg= | ||
|max takeoff weight note= | |max takeoff weight note= | ||
|fuel capacity= | |fuel capacity= | ||
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--> | --> | ||
|eng1 number=1 | |eng1 number=1 | ||
|eng1 name= | |eng1 name= Nanda E-5 | ||
|eng1 type= | |eng1 type=Twin row, 14-cylinder air cooled radial engine | ||
|eng1 kw=<!-- prop engines --> | |eng1 kw=<!-- prop engines --> | ||
|eng1 hp= | |eng1 hp= | ||
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|eng1 kn=<!-- jet/rocket engines --> | |eng1 kn=<!-- jet/rocket engines --> | ||
|eng1 lbf=<!-- jet/rocket engines --> | |eng1 lbf=<!-- jet/rocket engines --> | ||
|eng1 note={{cvt| | |eng1 note={{cvt|902|PS|kW hp|0}} | ||
|prop blade number= | |prop blade number=3 | ||
|prop name= | |prop name=metal constant-speed propellers | ||
|prop dia m=3 | |prop dia m=3 | ||
|prop dia note= | |prop dia note= | ||
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Performance | Performance | ||
--> | --> | ||
|max speed kmh= | |max speed kmh=455 | ||
|max speed note=at {{cvt|7000|m|0}} | |max speed note=at {{cvt|7000|m|0}} | ||
|cruise speed kmh= | |cruise speed kmh= | ||
|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=1201 | ||
|range note= | |range note= | ||
|combat range km= 1144 | |combat range km= 1144 | ||
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|ferry range note= | |ferry range note= | ||
|endurance=<!-- if range unknown --> | |endurance=<!-- if range unknown --> | ||
|ceiling m= | |ceiling m=10000 | ||
|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| | |time to altitude={{cvt|3000|m|0}} in 3 minutes 35 seconds | ||
|wing loading kg/m2= | |wing loading kg/m2= 93.8 | ||
|wing loading note= | |wing loading note= | ||
|fuel consumption kg/km= | |fuel consumption kg/km= | ||
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--> | --> | ||
|guns=<br/> | |guns=<br/> | ||
:* | :* 4 × {{cvt|7.7|mm|3}} [[Shrev 97 machine gun]] | ||
|bombs=<br/> | |bombs=<br/> | ||
2 x 30 kg (66 lb) bombs or 1 x 160-litre (42.27 US gallon drop tank)<br/> | |||
|avionics=[[Kol 89]]Z radio | |avionics=[[Kol 89]]Z radio | ||
}} | }} | ||
Revision as of 05:39, 20 September 2020
| 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 Air Force |
| 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 Mitsubishi V6K "Pujyam".
Design and Development
Operational History
Variants
Operators
Specifications (Mahindra V5K4)
General characteristics
- Crew: 1
- Length: 7.565 m (24 ft 10 in)
- Wingspan: 11 m (36 ft 1 in)
- Height: 3.27 m (10 ft 9 in)
- Wing area: 17.8 m2 (192 sq ft)
- Empty weight: 1,300 kg (2,866 lb)
- Gross weight: 1,750 kg (3,858 lb)
- Powerplant: 1 × Nanda 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: 455 km/h (283 mph; 246 kn) at 7,000 m (22,966 ft)
- Range: 1,201 km (746 mi; 648 nmi)
- Combat range: 1,144 km (711 mi; 618 nmi) 575
- 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 × 7.7 mm (0.303 in) Shrev 97 machine gun
- Bombs:
2 x 30 kg (66 lb) bombs or 1 x 160-litre (42.27 US gallon drop tank)
Avionics
Kol 89Z radio