| UAV Name | Short Range - Tunder SR |
| Uses | Target Drone, Missile evaluation and testing |
| Power Plant | 25~30 hp two stroke, gasoline |
| Dimensions | Length 2.83m, Wingspan 3.05m (Delta wing) |
| Weight | Max. takeoff weight 68 kg |
| Performance | Speed: 300 kph; Endurance: 1.5 hr; Range: 5~10 km (optically tracked) |
| Payload | Upto 16 smoke or IR flares (or a combination) |
| Guidance Tracking | Remote control/Optical Tracking |
| Launch | Catapult launcher |
| Recovery | Parachute/Belly landing |
| Structural Composition | Composites |
| GCS | N/A |
| Datalink | Command Link |
| ElectricalPower | N/A |