| Projects | Nominal Value | Remarks |
| Launch platform | individual portable canister launch or vehicle multiple launcher launch | |
| Max range | <10km | |
| Accuracy | CEP 1.5m for 4m×6m targets | |
| Power plant | electric | |
| Main flight performance specifications | Endurance: 40~50min | |
| Typical operation altitude: 50~500m |
| Flight speed: 30~55 m/s |
| Turning radius: 100m |
| Wind resistance: level 6 |
| Structure specifications | Takeoff weight: 10kg | |
| Missile plus canister weight: 13kg |
| Canister dimension (L×W×H): 1050×140×140 mm |
| Configuration: tandem wing |
| Warhead and fuze | Warhead: HE warhead, weight 1.5 kg | |
| Fuze: dual environment force full safety electromechanical fuze |
| Control and guidance | Guidance: integrated navigation of INS and SATCOM, terminal guidance is strapdown imaging guidance | visible light single mode |
| Control: program control autonomous flight and man-in-loop remote control | |
| Launch preparation time | 5min | |
Loitering UAV
