The Flight Stand 60 Engine Test Stand is a precision-engineered solution designed for performance validation of UAV propulsion systems in demanding test environments. With a thrust capacity of up to 60 kgf and torque measurement to 30 Nm, it provides high-fidelity data across the entire performance envelope of turbine and piston engines. The system supports peak RPM measurements up to 16,800 and includes integrated monitoring of fuel flow (up to 800 mL/min) and exhaust gas temperature up to 800°C, ensuring comprehensive evaluation during full-power and transient load conditions.

Tailored for laboratory and field deployment, the Flight Stand 60 features robust environmental tolerance, operating within 0°C to 40°C and 20%–80% relative humidity. Its plug-and-play configuration includes 9V, 2A power support via wall-mounted AC-DC adapters, allowing seamless integration into existing test setups. Built for unmanned systems engineers, the platform ensures consistent, real-time feedback during propulsion development, durability testing, and pre-deployment qualification.