Overview
The HAL Tejas is a light multirole fighter developed in India. Entering service in the 2010s, it represents a major domestic aerospace effort. The aircraft replaces older fighters in Indian Air Force service.
Specifications
Units
- Engine
- 1 × General Electric F404-GE-IN20
- Engine type
- Turbofan
- Thrust
- 20,200 lbf · 90 kN
- Avionics
- NVG & HUD by CSIO and SSDU & ADC by Bharat Electronics Limited
- Wing tips
- No winglets
- Seats
- 1
- Crew
- —
- Cabin width
- —
- Cabin height
- —
- Cabin length
- —
- Exterior length
- 43 ft 4 in · 13.20 m
- Tail height
- 14 ft 5 in · 4.40 m
- Fuselage diameter
- 3 ft 3 in · 1.00 m
- Wing span
- 26 ft 11 in · 8.20 m
- Baggage volume
- —
- Gross weight
- —
- Empty weight
- —
- Max takeoff weight
- 29,800 lb · 13,500 kg
- Max landing weight
- —
- Max payload
- 11,700 lb · 5,300 kg
- Fuel capacity
- 1,620 gal · 6,100 L · 4,900 kg (Jet A)
- Max cruise speed
- 1,066 kt · 1,227 mph · 1,974 km/h
- Maximum speed
- —
- Cruise speed
- —
- Approach speed
- —
- Range
- 1,726 nm · 1,990 mi · 3,200 km
- Fuel burn
- —
- Ceiling
- 50,000 ft · 15,200 m
- Rate of climb
- —
- Takeoff distance
- —
- Landing distance
- —
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