| Operation Range | 80 km – 100 km* radius |
| Takeoff Weight | 19 kg – 30 kg depends on configuration |
| Endurance | up to 8+ hours |
| Wingspan | 4 m |
| Body Length | 2.2 m |
| Tail Height | 0.5 m |
| Total Height | <1 m |
| V Loitor | 53 kn |
| V Max | 75 kn |
| V Stall | 42 kn |
| Mission Altitude | up to 3500 ft AGL |
| Service Ceiling | up to 15000 ft ASL** |
| Takeoff System | Pneumatic Launcher |
| Landing System | Parachute / Net & Belly Landing* |
| Payload (EO) | AGS100 or AGS200 or up to 4 kg payload with 150 W |
| Datalink | Digital (FDM) 8W, up to 80 km radius |
| Encryption | Crypto* |
| Backup Power | Battery (>50 W) |
| Engine | 1-Cylinder (55cc)*** |
| Ignition | Electronic |
| Fuel Type | Unleaded Gasoline |
| Fuel Capacity | up to 10kg |
| Propulsion | Pusher Propeller |
| Ignition | Manual Electric Starter |
| Design Environment | -20°C – +65°C, Environmentally sealed*, Splash Salt Water Resistant*, Float on ditch* |
| Transport | Rugged Composite Transport Case |
* Optional
** Depends on configuration
*** Modified for aviation and performance