SPARTAN is a coaxial Group 2 UAS developed for medium-lift logistics, mapping, and multi-role defense missions requiring dependable performance in demanding conditions. The platform supports payloads up to 15.3 lbs within a 30-lb maximum takeoff weight, providing a balance between portability and lift capability. Its cylindrical architecture reduces mechanical complexity while supporting durability, enabling consistent operation in harsh operational environments. Designed for team-based deployment, the system aligns with field logistics requirements where rapid setup, transportability, and mission adaptability are essential.
The aircraft incorporates a universal click-ring interface that allows rapid payload exchange or integration of mission-specific equipment without structural modification. With endurance exceeding 70 minutes in ideal configurations and speeds above 65 mph, SPARTAN enables extended-area operations and efficient coverage of large operational zones. The airframe is engineered for all-weather use, with resistance to rain, dust, snow, and high winds, while maintaining stable flight characteristics. Its autonomy-ready framework supports integration with advanced control systems, reducing operator workload and enabling scalable deployment across defense operations that demand flexible, modular unmanned capabilities.
Specifications:
| Dimensions (L x D): | 771 x 147 mm (30.4 x 5.8 in) |
| Weight: | 2.7 kg (5.95 lbs) – no battery or payload |
| MTOW: | 13.6 kg (30 lbs) |
| Payload Capacity: | One battery: 6.9 kg (15.3 lbs) Dual battery: 3.9 kg (8.7 lbs) |
| Flight Endurance: | One battery: 20 minutes with max payload Dual battery: 65+ minutes with no payload (50 min. w/ 7.5 lbs. payload) |
| Max Speed: | Manual: 60+ mph (27 m/s)
Auto: 40 mph (18 m/s) |
| Max Altitude: | 5000 m (14,600 ft) |
| Data Link: | Standard configuration 2.4 GHz |
