MTS06 Motor Test Stand
Thrust Force
With MTS06, fixed wing / multicopter UAV engines can be tested up to 6 kg thrust.
Universal Engine Compatibility
Compatible with electric motors in the motor diameter range 10-44 mm.
Precision Measurement
Accurate results with 95% accuracy with MTS06.
Propeller
Possibility to test up to 13" different propeller options.
MTS06 Technical Specifications
The Minimal Thrust Test System is designed to test the performance of BLDC engines. With MTS06, thrust, energy consumption, speed, engine life and temperature data can be obtained. At the same time, the battery and engine driver (ESC) used in unmanned aerial vehicles can be included in the system, enabling electronic and propulsion system testing before flight tests.
With MTS06, different engine and propeller combinations can be tested and flight time can be increased up to 30%.
MTS06 offers the opportunity to perform tests manually and automatically with specially developed computer-aided control software.
Test results are saved in folders for easy access.
| Dimensions | |
| Propeller | max 13″ |
| Thrust Force | max 6 kg |
| Current | 100 A |
| Voltage | 60 V |
| Engine Speed | 35000 RPM |
| Temperature | -50°C/200°C |
| Manual Control | ✓ |
| Automatic Control | No |
| Feedback | No |
| Wifi Connection | No |
| Operating Temperature | -10°C/50°C |
Automatic Test Modes
Flight simulation test. Endurance test. Thrust controlled test. PWM controlled test.
Feedback Feature
Flight time and speed estimation. Efficiency analysis. Limit analysis. Suggestions for improvement.
Real Time Graphics
Possibility to follow real-time graphics during the test.
Automated Reporting
Possibility to record and analyze test results in .csv format thanks to report and graph output.
Minimal Thrust Test System Software
Real-time dynamic testing with our computer-controlled software.
Manual and Automatic Control
High Accuracy Rate
Reporting and Feedback Feature
Fast and Advanced Interface
Real Time Graphics
Data Output Format .CSV
