BREAK THE GRAVITY
NOX-40S lifts payload like gravity doesn't exist. Built by Ungravity Republic. For your unit.
About Us
UNGRAVITY REPUBLIC is a defense-tech company building strike unmanned systems. Multi-role platforms that adapt to new challenges under the demands of modern war — here and now. We're breaking a rule once thought unbreakable: that weight defines what's possible. Now critical payload reaches places conventional methods can't.
NOX-40S
NOX-40S is a heavy multi-purpose Vertical Takeoff and Landing (VTOL) unmanned aerial system with a payload capacity of up to 30 kg.
The system is designed to perform logistics, reconnaissance, and strike missions at ranges of up to 20 km. It is equipped with an intuitive FPV-style control system, a Starlink communication channel, an integrated payload release mechanism, and electro-optical surveillance equipment.
The system can be prepared for operation in up to 15 minutes, enabling rapid deployment in field conditions. It can operate across a wide range of weather conditions and supports automatic, semi-automatic, and manual flight modes.
- Payload capacity of up to 30 kg.
- Tactical operational radius of up to 20 km.
- Starlink integration.
- Integrated payload release system.
- FPV-based control interface.
- Ready for operation in 15 minutes.
- Reliable performance across a wide temperature range.
- Optional thermal imaging module.
| Parameter | Value |
|---|---|
| Type | Multi-purpose VTOL quadcopter |
| Class | Tactical strike UAS |
| Takeoff / Landing Type | Vertical |
| Parameter | Value |
|---|---|
| Maximum Flight Range | Up to 20 km |
| Tactical Operational Radius | 20 km |
| Maximum Speed | 60 km/h |
| Cruise Speed | 54 km/h |
| Operating Altitude | 300 m |
| Maximum Altitude | 1,000 m |
| Flight Time (without payload) | Up to 60 min |
| Flight Time (with maximum payload) | At least 40 min |
| Maximum Wind Speed for Operation | Up to 8 m/s |
| Parameter | Value |
|---|---|
| Maximum Payload Capacity | 30 kg |
| Maximum Takeoff Weight | 112 kg |
| Communication System | Starlink |
| Payload Release System | Integrated |
| Strike Accuracy | CEP not exceeding 3 m |
| Probability of Target Engagement | At least 0.8 |
| Parameter | Value |
|---|---|
| Camera | Daylight camera with optical zoom |
| Thermal Imaging Camera | Optional |
| Day Camera Resolution | 1920 × 1080 |
| Thermal Camera Resolution | Minimum 640 × 480 |
| Vehicle Detection Range | Up to 300 m |
| Human Target Detection Range | Up to 100 m |
| Parameter | Value |
|---|---|
| System Deployment Time | 15 min |
| Turnaround Time for Next Mission | Up to 15 min |
| Dimensions (L × W × H) | 1735 × 1735 × 940 mm |
| Power Supply | Li-Ion / LiPo 18S 73 Ah |
| Operating Temperature Range | -10°C to +40°C |