Mohajer (UAV) Specifications
| Mohajer-2 | Mohajer-6 | Mohajer-10 | |
|---|---|---|---|
| Country of Origin | Iran | ||
| User Countries/Groups | Iran, Hezbollah (Mohajer-4) | ||
| Builder | Qods Aviation Industries | ||
| Physical | |||
| Length | 2.9 m | 5.67m | |
| Wingspan | 3 m | 10m | 10m |
| Weight, Empty | |||
| Weight, Maximum | 85 kg | 600kg | 1000kg? |
| Performance | |||
| Engine | |||
| Maximum speed | 200 km/h | 200 km/h | 210 km/h |
| Cruising speed | |||
| Ceiling | 11,000 ft | 18,000ft | 20,000ft |
| Surveillance radius | 50 km | 200km | 2000km |
| Endurance | 90 minutes | 12hrs | |
| Launch | Pneumatic or jet-assisted | runway | |
| Recovery | By Parachute | runway | |
| Armament/Payload | Video and infrared cameras providing 1-meter resolution from altitudes up to 5,000 ft |
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