Name: Flight Stand 60
Availability: InStock

Сфера застосування

Тип 

Стан

Thrust

Torque

Fuel flow

Temperature

Northern America

Canada

Precision Engine Test Stand for High-Performance UAV and Defense Propulsion Systems. The Flight Stand 60 by Tyto Robotics is a high-accuracy engine test stand engineered for evaluating propulsion systems used in unmanned aerial vehicles and defense-grade platforms. Capable of capturing thrust up to 60 kgf and torque up to 30 Nm at 16,800 RPM, the system features a 1,000 Hz data acquisition rate for detailed dynamic analysis including harmonics, vibration signatures, and torque ripple—essential for validating mission-critical hardware. Designed around an ASTM E74/E2624-calibrated load cell, the platform delivers unmatched measurement fidelity in demanding R&amp;D environments.Equipped with a Python-controllable API and robust I/O, the Flight Stand 60 supports real-time integration with auxiliary sensors and actuators, offering seamless automation for powertrain mapping, carburetor tuning, or fuel endurance testing. Its software environment allows both manual and programmable control modes, empowering engineers to simulate complex mission scenarios and extract multidimensional performance data such as system efficiency, airspeed correlation, and 3D engine behavior. Whether you're optimizing crank angles or evaluating variable-pitch propellers, the Flight Stand 60 delivers laboratory-grade insights under operationally realistic conditions.

The Flight Stand 60 is a precision propulsion test stand from Tyto Robotics capable of measuring up to 60 kgf of thrust and 30 Nm of torque at up to 16,800 RPM, with a 1,000 Hz data acquisition rate for detailed dynamic analysis of harmonics, vibration signatures, and torque ripple. Its ASTM E74/E2624-calibrated load cell provides laboratory-grade measurement fidelity suited to validating UAV and defense propulsion hardware.

A Python-compatible API and flexible I/O enable real-time automation and integration with auxiliary sensors, supporting powertrain mapping, fuel endurance testing, carburetor tuning, and variable-pitch propeller evaluation. The software environment supports both manual and programmable control modes, allowing engineers to simulate complex mission scenarios and extract multidimensional performance data across the full operating envelope of electric, gasoline, and hybrid propulsion systems.

Flight Stand 60

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