| Length | 3200 mm |
| Wingspan | 1600 mm |
| Power System | Turbojet Engine |
| Takeoff and Landing Mode | Rocket-Assisted Launch/Parachute Recovery |
| Payload | ≥ 15 kg |
| Maximum Flight Range | ≥ 500 km |
| Minimum Flight Altitude | >20 m (Over Sea) / 50 m (Over Land) |
| Control Radius | 100 km |
| RCS | ≈0.1 square meters (X/Ku band, forward ±30°), and can be equipped with a Luneburg lens to increase the RCS value to 2~3 square meters |
| Maneuverability | Stable Banked S-Turn, Heading 180 Degrees + Dive |
| Maximum Level Flight Speed | ≥ 200 m/s |
| Maximum Takeoff Weight | ≥ 80 kg |
| Endurance | ≥ 1.2 h |
| Ceiling | ≥ 9000 m |
| Wind Resistance | Level 5 |
| Maximum Maneuvering Overload | ≥ 5 g |
| Number of UAV in The Sky Simultaneously | ≥ 30 |