The LM8 A (Pneumatic Version) is a loitering munition drone with 120 kg maximum takeoff weight, 1,000+ km flight range, and 5–6 hour endurance powered by a 17 kW gasoline engine.
Key Capabilities
- Pneumatic catapult launch system
- 120 kg maximum takeoff weight with 30 kg payload
- 1,000+ km maximum flight range
- 5–6 hour maximum endurance time
- 180 km/h maximum speed with 165 km/h cruise
- 92 gasoline fuel with 40 L tank capacity
- Operating temperature: -25°C to 60°C
- 350 m minimum turning radius
Technical Specifications
| Maximum load capacity | 30 kg |
|---|---|
| Maximum takeoff weight | 120 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 | >1,000 km |
| Maximum endurance time | 5–6 h |
| Cruise fuel consumption | ≈7 L |
| Fuel type | 92 gasoline |
| Fuel tank capacity | 40 L |
| Engine parameters | 17 kW |
| Takeoff method | Pneumatic catapult |
Applications
Long-range loitering munition operations, extended surveillance and strike, area denial, and tactical missions requiring extended loiter time.
Deployment note: Final configuration, operator training, airspace approval, and local regulatory compliance are required before deployment.
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