Phoenix E
An advanced AI-enabled UAV system designed for long-range precision strikes with minimal operator input and maximum mission impact
Data-link Redundancy
Dual redundant datalinks ensure maximum mission continuity — preserving command, control and sensor data even during aggressive communications jamming.
Optional EW Resilience
For advanced operators working in complex, contested environments, the Phoenix E offers an optional add-on that provides full resilience to GPS jamming and spoofing — combining adaptive antennas with visual-inertial navigation to maintain navigation and mission continuity.
Long Endurance
Class-leading endurance — up to 3 hours in light configuration or 2.5 hours with a full mission payload, setting a new benchmark in its category.
Actively Cooled Motor Systems
Actively cooled ESCs and motors enable the Phoenix E to maintain hover for as long as energy allows — providing continuous thermal management for critical components during sustained vertical flight.
Ultra Quick and Simple Assembly
A screwless (zero-screw) design enables complete assembly of the Phoenix E in the field without a screwdriver — delivering an ultra-quick setup process and significantly reducing expedition time. This tool-free architecture also simplifies O-level maintenance, making routine inspections and swaps faster, safer, and more user-friendly.
Dual Payload Capable
The Phoenix E is capable of carrying two payloads simultaneously, enabling operators to perform ISR and 3D mapping missions on the same sortie - maximizing operational efficiency and mission versatility without the need for reconfiguration.
Mini Cargo Carrier Capability
Optional wing pylons and quick-release mechanisms give operators the capability to carry and deploy munitions or FPV drones seamlessly — without requiring any additional structural or system modifications.
Unmatched Hovering Time
While most VTOL UAVs are limited to 4–5 minutes of hover using dedicated lift batteries, the Phoenix E can remain in hover for up to 45 minutes, empowering operators to execute precise, sensitive, and extended remote operations with unmatched stability.
Specifications
| Configuration | Fixed Wing Electric VTOL |
|---|---|
| Endurance | ~2.5 Hrs. (160 Min) |
| Optimized Cruise Speed (VR) | 32 Knots (16 m/s) |
| Stall speed (Vstall) | 20 Knots (10 m/s) |
| Service Ceiling | 10,000 ft. ASL |
| Optimized Operational Alt. | 2,500 ft. ASL |
| Max Pitch Angle (flight) | 25 Degrees |
| Range (Comm. Limited) | 70 km. |
| T/O LND Method | Vertical (VTOL) |
| Max. Continuous Hover Time | 28 Min |
| Operating Temperature | -20°C to +50°C |
| Wingspan | 3,600 mm |
|---|---|
| Length | 1,900 mm |
| Empty Weight (No Batt.) | 22.6 Kg. |
| Max Takeoff Weight | 34 Kg. |
| Max Payload | 5 Kg. |
| Battery Weight | 6.8 Kg. |
| Box Dimensions (Folded) | 1,980mm x 920mm x 920mm |
| Shipping Weight | 52 kg. |
| Configuration | Mobile Rugged 19" Ground Control Station |
|---|---|
| Display | 19" LG Display |
| Resolution | 1440x900 |
| Auxiliary Bays | 3 |
| Sound | Active |
| Working Environment | -20°C to +50°C |
| Embedded Computer | onLogic Intel COMET lake i9 QUAD |
| GCS Dry Weight | 16 Kg. |
| Formats | SBAS, PPM, SERIAL |
| Control Method | PWM / TTL / S.BUS / TCP(IP output) |
| Primary | C-Band 5.8Ghz |
|---|---|
| Secondary | 2.4Ghz |
| Primary Comm. Antennas | 2 |
| Secondary Comm. Antennas | 1 |
| Ground Antenna (STD) | Omni-Directional Single Axis Antenna |
| Ground Antenna (Optional) | Omni-Directional Parabolic 2 Axis 360 Degrees Antenna |
| Ground Antenna Setup | Tripod |
