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ADA 'Tejas' resources

Author : B.Harry, updated 27 / 02 / 07

 

Recommended Resolution : 1024 x 768 pixels 

Recommended Reading : http://www.bharat-rakshak.com/IAF/Info/Aircraft/Tejas-Radiance.pdf

Recommended viewing : http://www.aeroindia.org/


 

This page attempts to document and archive developmental data and photographs of the "Tejas", Light Combat aircraft, being developed by the Aeronautical Development Agency (ADA) of India. At the the time of writing, there are two technology demonstrators and three Prototype vehicles undergoing flight testing. The latter two Prototype Vehicles (PVs), PV-2 and PV-3, represent production standard aircraft. Three aircraft, TD-1, TD-2 and PV-3 were the main attractions at Aero India 2007 and put up stunning aerobatic displays.

 

1.1 Photo Gallery (2007)  

 

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Tejas Prototype Vehicle (PV) - 3, Kh-2005; FILE : 1593 x 1062 / 289 KB

The aircraft is piloted by Grp.Capt. N. Harish ; FILE : 1600 x 1067 / 387 KB

 
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Kh-2001, the first Technology demonstrator ; FILE : 1280 x 790 / 162 KB Kh-2005 and Kh-2002 ; FILE : 1024 x 736 / 110 KB

 
Kh-2005 ;   FILE : 1600 x 1067 / 100 KB

Kh-2002 ;   FILE : 1600 x 1047 / 100 KB

 

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Tejas fiberglass mockup ; FILE : 1280 x 960 / 363 KB FILE : 1600 x 1067 / 470 KB
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FILE : 1280 x 853 / 220 KB The HJT-36 and the Tejas share a number of common LRUs ; FILE : 1600 x 989 / 361 KB
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FILE : 1600 x 1067 / 376 KB Tejas and Mirage-2000H comparison ; FILE : 1600 x 1067 / 424 KB
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Tejas with Jaguar upgrade DARIN-II. The latter derives some elements from the LCA programme; FILE : 1600 x 1067 / 379 KB Tejas TD-1, Kh-2001 ; FILE : 1600 x 1067 / 377 KB
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FILE : 1024 x 745 / 90 KB The Tejas contrasted against the MiG-35 ; FILE : 1280 x 960 / 290 KB

 
1.2 Tejas Trainer
 

The Tejas Trainer differs from the single-seat variant in many characteristics including the following,

  • Drooped Nose for better visibility from the rear seat.
  • Increase in empty weight by 161 kgs
  • Marginal decrease in internal fuel (~200 kgs)
  • Podded gun instead of internal gun (Gsh-23)
  • Mechanically linked control stick, rudder and throttle in rear cockpit
  • Basis for the Naval variant of the Tejas

 

Click to Expand

Click to Expand

 
Scanned image : 960 x 618 / 286 KB / 1200 dpi Scanned image : 978 x 600 / 288 KB / 1200 dpi  

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Scanned image : 800 x 507 / 215 KB / 1200 dpi Scanned image : 800 x 508 / 96 KB / 1200 dpi  
1.3 Documents, Literature and Misc equipment

Antenna diameter 650 mm  
Antenna gain 33 dB
TWT Power Output 6.5 kW (increaseable to 10 kW, 10% duty cycle)
Range 120 km against 2 sq.m RCS aerial target, >150 km for surface targets against sea clutter
All Up Weight (AUW) 130 kg
  To keep the radar up to evolving standards, a new Advanced Signal and Data Processing Unit based upon Power-PC chips, has been developed to replace the older unit.
LRDE/HAL Multi-Mode Radar for LCA ; FILE : 1024 x 768 / 282 KB    

Click for high-res version

Click to download hi-res version

 
Voice Command / VTAS Unit for the Tejas cockpit. This unit has been developed by the Aeronautical Developmetn Establishment (ADE) of DRDO. This unit has also been developed by the Aeronautical Developmetn Establishment (ADE) of DRDO  
 

Not expansible

 

 
The second unit of the 8 Limited Series Production (LSP) aircraft, under assembly.    

 

 
 

 


 

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