SOUTH ASIA
 

Country

  Prime Manu.
  UAV Designation
Production status  
Operational status 
Power plants
Dimensions (m)            
  Wieghts (kg)  
        Performance      
Comments
 Development
Production
Operation
 Purpose
Mission payload
Launch, take-off type
Recovery, landing type
Min crews need
System composite
Datalink, comm frequency
Engine
Propulsion
Wing span
Wing area (㎡)
Length overall
Height overall
Wheel track
Wheel base
Wing aspect ratio
Fuselage max width
Weight empty
Max fuel weight
Max Payload
Max T-O/launch weight
Max level speed (kt)
Cruising speed (kt)
Loiter speed (kt)
Stall speed (kt)
Service Ceiling (ft)
Max rate of climb (ft/min)
Range (nm)
Max Endurance (h)
India
ADE

Kapothaka

Complete

Complete

Deployed

Concept validation UAV.

Can include Luneberg lens and/or cornor reflectors for radar signature enhancement, smoke generators, IR flares, and miss-distance indicator.

Rocket boost

Two-stage parachute deployment to airbag landing.

 

GCS

UHF

One 26 hp two-cylinder two-stroke engine.

Two-blade pusher prop.

4.50

 

3.60

 

 

 

 

 

 

12

20

125

97

 

 

43

9,840

 

16.2

1.5

 

Nishant
Complete Underway Limited

Reconnaissance, surveillance and target acquisition UAV

Day/night sensors.

Mobile hydraulic/pneumatic catapult.

Parachute and airbag recovery to belly landing.

 

GCS

Real time; ECM-hardened digital D-band.

Rotary  

6.50

 

4.60

1.183

      132

252

  60 350

108

73

    13,100   54 4.0  
Lakshya

Complete

underway

Deployed

             

turbojet

                       

350kg

           

600km

 

RPV & Missile

EO,IR,Radar

Country

  Prime Manu.
  UAV Designation
Production status  
Operational status 
Power plants
Dimensions (m)            
  Wieghts (kg)  
        Performance      
Comments
 Development
Production
Operation
 Purpose
Mission payload
Launch, take-off type
Recovery, landing type
Min crews need
System composite
Datalink, comm frequency
Engine
Propulsion
Wing span
Wing area (㎡)
Length overall
Height overall
Wheel track
Wheel base
Wing aspect ratio
Fuselage max width
Weight empty
Max fuel weight
Max Payload
Max T-O/launch weight
Max level speed (kt)
Cruising speed (kt)
Loiter speed (kt)
Stall speed (kt)
Service Ceiling (ft)
Max rate of climb (ft/min)
Range (nm)
Max Endurance (h)
PAKISTAN
AWC

MkⅠ

Complete

Complete

Underway

Low-cost surveillance and target acquisition UAV.

An 8 mm CCD colour TV camera with a 120 mm motorised zoom; optional alternative is a FLIR sensor.

Conventional wheeled take-off, or rocket booster assistance.

Conventional wheeled landing, or with parachute recovery.

Two-axis autopilot with height hold. GCS housed in 6.10 m shelter with workstations for pilot, commander and photo interpreter. Sky Tracker for piloting and mission planning; Sky Navigator with moving map display.

50 W uplink, 18 W downlink.

Single 100 cc piston engine.

A two-blace tractor prop.

2.74

 

2.13

         

16

7 liters

14

30

94

59

49

 

9,840

 

16.2

2

 
   

In  service in Parkistan Army since 1997

                                                     

Mk Ⅱ

Complete

Underway

Underway

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Two single 100cc piston engine

 

3.66

 

2.74

         

26

20 liters

34

60

94

70

49

 

13,120

 

27

3

 

1999

                                                               

Mk Ⅲ

Underway

Underway

 

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