Mohajer (UAV)
| Specifications (Mohajer-2) | |
|---|---|
| Country of Origin | Iran |
| User Countries/Groups | Iran, Hezbollah (Mohajer-4) |
| Builder | Qods Aviation Industries |
| Physical | |
| Length | |
| Wingspan | 3 m |
| Weight, Empty | |
| Weight, Maximum | 85 kg |
| Performance | |
| Engine | |
| Maximum speed | 200 km/h |
| Cruising speed | |
| Ceiling | 11,000 ft |
| Surveillance radius | 50 km |
| Endurance | 90 minutes |
| Launch | Pneumatic or jet-assisted |
| Recovery | By Parachute |
| Other | |
| Armament/Payload | Video and infrared cameras providing 1-meter resolution from altitudes up to 5,000 ft |
