Flat Wing Aspect Ratio
6.03
Entry Into service
1968-01-01
Maximum Take-Off Weight
4.235 t (paragliders: kg)
Pictures
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Aircraft Weight Variants
| Aircraft |
Maximum Take-Off Weight (t (paragliders: kg)) |
Total Fuel Capacity |
|
HAL HJT-16 Kiran |
4.235 |
1137 |
Similar airplanes
All data (28 fields)
- Name
- HAL HJT-16 Kiran
- Manufacturer
- Hindustan Aeronautics Limited
- Description
- The HAL HJT-16 Kiran () is an Indian two-seat intermediate jet-powered trainer aircraft designed and manufactured by aircraft company Hindustan Aeronautics Limited (HAL).
- First Flight
- 1964-09-04
- Entry Into service
- 1968-01-01
- Production End
- 1989-01-01
- Designer
- Hindustan Aeronautics Limited
- Type
- Intermediate jet trainer
- Length (m)
- 10.6
- Height (m)
- 3.64
- Cockpit Crew
- 2
- Max Speed (km/h)
- 695
- Cruise Speed (km/h)
- 324
- Min Speed (km/h)
- 137
- Max Ceiling (m)
- 9150
- Armament
- two 500lb (227kg) bombs or two SNEB rocket pods containing seven 68 mm rockets or two pods with 7.62 mm machine guns, or two 50-Imp Gal (226 litre) drop tanks
- Endurance (h)
- 1
- National Origin
- India
- Number Built
- 190
- Powerplant Description
- 1 × Rolls-Royce Viper 11 turbojet, 11.12 kN thrust each
- Primary Users
- Indian Air Force, Indian Navy
- Status
- In service
- Wikipedia Article (URL)
- en.wikipedia.org/wiki/HAL_HJT-16_Kiran
- Flat Wing Span (m)
- 10.7
- Flat Wing Area (m²)
- 19
- Flat Wing Aspect Ratio
- 6.03
- Aircraft Engine
- Armstrong Siddeley Viper
- Number of Engines
- 1