HAL Tejas Mk2

Airplanes

Length

14.65 m

Flat Wing Span

8.5 m

Height

4.87 m

Max Mach

1.8 Mach

Max Ceiling

17300 m

Number of Engines

Aircraft Engine

Maximum Take-Off Weight

17.5 t (paragliders: kg)

Maximum Range

3000 km

Pictures

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Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Maximum Range (km)
HAL Tejas Mk2	17.5	3000

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)
Dassault Mirage 2000		14.36	9.13	Compare
Dassault Mirage F1		15.3	8.4	Compare
IAI Lavi	Pratt & Whitney PW1120	14.57	8.78	Compare
IAI Kfir	General Electric J79	15.65	8.22	Compare
Saab JAS 39 Gripen	Volvo RM12	14.9	8.4	Compare
Convair Model 200		15.5448	8.2296	Compare

All data (17 fields)

Name: HAL Tejas Mk2
Manufacturer: Hindustan Aeronautics Limited
Description: The HAL Tejas Mark 2 (), or Medium Weight Fighter (MWF), is an Indian 4.5 generation, single-engine, canard delta wing, multirole combat aircraft designed by the Aeronautical Development Agency in collaboration with Aircraft Research and Design Centre (ARDC) of Hindustan Aeronautics Limited for the…
Designer: Hindustan Aeronautics Limited
Length (m): 14.65
Height (m): 4.87
Max Ceiling (m): 17300
Armament: 1 × 30 mm GSh-30-1; 13 hardpoints with a capacity of around 6.5 tonnes (expected), with provisions to carry combinations of :; Air-to-air missile :; MICA (planned); ASRAAM; Meteor (planned); Astra; NG-CCM (planned); Air-to-surface missile :; BrahMos-NG ALCM; LR-ALCM (planned); Rudram 2/3 (planned); SCALP-EG (planned); Crystal Maze; Anti-radiation missile :; Rudram 1/2 (planned); Bombs:; Precision…
Max Mach (Mach): 1.8
National Origin: India
Powerplant Description: 1 × General Electric F414-INS6 afterburning turbofan with FADEC
Primary Users: Indian Air Force (intended)
Status: Prototype development
Wikipedia Article (URL): en.wikipedia.org/wiki/HAL_Tejas_Mk2
Flat Wing Span (m): 8.5
Aircraft Engine: General Electric F414
Number of Engines: 1