Product Description
OVERVIEW
CH-804 UAV system is a mature product with convenient operation and strong expansion capability. It adopts propelled, monoplane and twin- tail boom conventional configuration. It is powered by mini-gasoline engine. It is taken off by catapult and recovered by parachute. The ground part of system is equipped with ground control cabinet system to conduct flight control, mission planning and loading, link monitor as well as information processing. The system is cost effective and is able to carry out the operations of system expansion and update.
CH-804 UAV focuses on performing tasks, such as combat surveillance, artillery correction, firepower guidance, destruction effectiveness assessment, providing information of battlefield situation, such as force deployment, target location, etc.
MAJOR FEATURES
- Long Endurance
- Flexible Loading and Carrying Capacity
- Wide variety of cutting edge payloads
- Rapid Deployment
- High Cost-effective Ratio
UAV SYSTEM COMPOSITION
TECHNICAL SPECIFICATIONS
| Take-off Mass | 21.5 kg |
| Payload Capacity | 4.8 kg |
| Endurance | 8 h (Distinctive endurance according to various loading) |
| Operation Radius | 75 km (LOS) |
| Max. Range | 800 km |
| Ceiling | 4,000 m |
| Cruising Altitude | 500-1,500 m |
| Cruising Velocity | 90-110 km/h |
| Max. Speed | 120 km/h |
| Deployment Time | ≤ 30 min |
| Withdrawal Time | ≤ 15 min |
| Launch | Catapult |
| Recovery | Parachute |