The LM8 B (Pneumatic Version) is a loitering munition drone with 130 kg maximum takeoff weight, 700+ km flight range, and 4-hour endurance powered by a 280CC 35HP gasoline engine.
Key Capabilities
- Pneumatic catapult launch system
- 130 kg maximum takeoff weight with 50 kg payload
- 700+ km maximum flight range
- 4-hour maximum endurance time
- 180 km/h maximum speed with 165 km/h cruise
- 280CC, 35HP gasoline engine
- 92 gasoline fuel with 30/40 L tank capacity
- Operating temperature: -25°C to 60°C
Technical Specifications
| Maximum load capacity | 50 kg |
|---|---|
| Maximum takeoff weight | 130 kg |
| Operating temperature | -25°C to 60°C |
| Minimum turning radius | 350 m |
| Climb rate | 4–5 m/s |
| Pitch angle | 15° |
| Roll angle | 30° |
| Cruise speed | 165 km/h |
| Maximum speed | 180 km/h |
| Maximum flight range | >700 km |
| Maximum endurance time | 4 h |
| Cruise fuel consumption | 8 L |
| Fuel type | 92 gasoline |
| Fuel tank capacity | 30 L / 40 L |
| Engine parameters | 280CC, 35HP |
| Takeoff method | Pneumatic catapult |
Applications
Heavy-payload loitering munition operations, extended-range strike, area denial, and tactical missions requiring enhanced payload capacity.
Deployment note: Final configuration, operator training, airspace approval, and local regulatory compliance are required before deployment.
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