technical specs
Q01 – MISSION-SPECIFIC MALE platform
| Weights & measurements | |
|---|---|
| MTOM | 2.750 kg |
| Max. payload | 600 kg, underwing stations 360 kg |
| Wing span | 20 m |
| Fuel | 2 x 256 kg = 512 kg inside wing |
| Height | 10' 11'' ft (3.33 m) |
| Length | 35' 3'' ft (10.7 m) |
| g-load | + 3.6/–1.44 |
| Performance data | |||
|---|---|---|---|
| Cruise speed to mission | 180 kt | ||
| Typical mission speed | 110 kt | ||
| Range manned | >1,350 nm, endurance >12 hrs | ||
Range unmanned | 4,500 nm, endurance >50 hrs | ||
| Service ceiling | 30,000 ft | ||
| Power plant | 6-cyl V, 3l, two turbocharger Technify Continental CD 310 hp JET A1 engine | ||
| Propeller | MT 3-blade constant speed prop |
| long endurance |
|---|
| Optional piloted flight control system |
| Manned & Unmanned (up to 50 hrs) |
| Two crew, provision for work share (+ rest/lavatory) |
Deploy (manned) to target area 3,000 nm in one step |