STRIKER
STRIKER ‘s aerodynamic airframe is optimized for higher cruise speeds, allowing it to cover mission areas faster while conserving fuel over long distance flights. Ground operators plan missions through a control interface, setting way points and payload configurations before launch, with the aircraft handling in flight adjustments on its own. The catapult launch system requires minimal ground infrastructure, allowing STRIKER to be deployed from confined or remote locations without a prepared runway. This field serviceable design makes it easy to redeploy across multiple mission sites with minimal turnaround time, keeping STRIKER ready for repeated long range missions.
Key Highlights
Description
Introducing STRIKER, a fixed wing unmanned aerial system (UAS) designed for long range autonomous flight. Built with a compact and durable composite airframe, it is capable of covering long distances while maintaining stable and reliable performance.
The platform features autonomous way-point navigation, encrypted telemetry for secure communication, and a modular payload bay that supports compatible cameras, sensors, and other mission equipment. Its catapult launch compatible design allows it to operate without a conventional runway, making deployment faster and more flexible in different environments.
With a combustion propulsion system, weather resistant construction, and up to 3 hours of flight endurance, STRIKERis suitable for applications such as environmental monitoring, disaster assessment, mapping and surveying, border and coastal observation, and logistics support, where extended flight time and dependable performance are important.
| Specification | Value |
|---|---|
| Maximum Take-off Weight (MTOW) | 20 kg |
| Payload Capacity | 5 kg |
| Empty Weight | Approximately 13 to 15 kg |
| Wingspan | 1250 mm |
| Length | 1600 mm |
| Cargo Volume | 3 L |
| Cruise Velocity | 45 m/s |
| Maximum Range | 100 km |
| Endurance | 3 Hours |
| Propulsion | Combustion Propulsion System |
Key Features
High Speed Aerodynamic Airframe
Catapult Launch Compatible Design
Modular Payload Bay
Autonomous Way-point Navigation
Encrypted Telemetry Communication
Weather Resistant Composite Structure
Combustion Propulsion System
Long Range Flight Capability
