SPIRIT is a small tactical UAS engineered to support ISR, inspection, and sensing missions across defense and security operations. Designed with a coaxial rotor configuration and cylindrical airframe, the platform delivers stable flight performance and efficient lift in confined and adverse environments. With a payload capacity of up to 6.5 lbs and a maximum takeoff weight of 13.5 lbs, it provides a balance of capability and portability for single- or two-operator deployment. Its rugged, all-weather construction enables consistent operation in rain, dust, snow, and high winds, ensuring mission readiness in unpredictable conditions.
Built around a modular open systems approach, SPIRIT features a universal click-ring payload interface that allows rapid integration or exchange of mission-specific sensors and equipment without redesign. The system is NDAA-compliant and recognized within the Blue UAS framework, aligning with defense acquisition and security requirements. With flight endurance of up to 53 minutes and speeds exceeding 60 mph, it supports extended operations while maintaining responsiveness in dynamic environments. Its autonomy-ready architecture allows integration with advanced control systems, enabling operators to scale capability, reduce fleet complexity, and adapt to evolving mission demands using a common platform.
Specifications:
| Dimensions (L x D): | 257 x 106 mm (12 x 4.2 in) – no battery or payload |
| Weight: | 1.8 kg (4.1 lbs) – no battery or payload |
| MTOW: | 6.1 kg (13.5 lbs) |
| Payload Capacity: | 3.0 kg (6.5 lbs.) |
| Flight Endurance: | Single battery: 38 minutes with no payload (16 minutes w/max payload) Two batteries: 53 minutes with no payload (32 minutes w/max payload) |
| Max Speed: | 60 mph (27 m/s) |
| Max Altitude: | 5000 m (14600 ft) |
