Entry Into service
2015-01-17
Maximum Take-Off Weight
13.5 t (paragliders: kg)
Pictures
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Aircraft Weight Variants
| Aircraft |
Maximum Take-Off Weight (t (paragliders: kg)) |
Total Fuel Capacity |
|
HAL Tejas |
13.5 |
3060 |
Similar airplanes
All data (24 fields)
- Name
- HAL Tejas
- Manufacturer
- Hindustan Aeronautics Limited
- Description
- The HAL Tejas () is an Indian single-engine, 4.5 generation, delta wing, multirole combat aircraft designed by the Aeronautical Development Agency and manufactured by Hindustan Aeronautics Limited (HAL) for the Indian Air Force (IAF) and the Indian Navy.
- First Flight
- 2001-01-04
- Entry Into service
- 2015-01-17
- Designer
- Hindustan Aeronautics Limited
- Type
- Multirole light fighter
- Length (m)
- 13.2
- Height (m)
- 4.4
- Cockpit Crew
- 1
- Max Speed (km/h)
- 2220
- Max Ceiling (m)
- 16000
- Armament
- 1 × 23 mm twin-barrel GSh-23 cannon with 220 rounds; 9
- Max Mach (Mach)
- 1.8
- National Origin
- India
- Number Built
- 45
- Powerplant Description
- 1 × General Electric F404-GE-IN20 afterburning turbofan with FADEC
- Primary Users
- Indian Air Force
- Status
- In service
- Wikipedia Article (URL)
- en.wikipedia.org/wiki/HAL_Tejas
- Flat Wing Span (m)
- 8.2
- Flat Wing Area (m²)
- 38.4
- Aircraft Engine
- General Electric F404
- Number of Engines
- 1