Disclaimer
Many aspects of the design process are not covered by this data, such as dynamic testing, PID and flight stability, endurance testing, noise and vibration, airspeed, temperatures, control protocols, calibration, and more. Because a data point exists at a high throttle for the component does not mean it can safely sustain this throttle for more than a few seconds. Go to the Tyto Robotics website to learn more about testing applications.
While our database provides valuable insights to help during the initial stage of component preselection, it only focuses on static test data. We strongly recommend validating all performance data by conducting your own internal testing before relying on this data for your design project.
Many aspects of the design process are not covered by this data, such as dynamic testing, PID and flight stability, endurance testing, noise and vibration, airspeed, temperatures, control protocols, calibration, and more. Because a data point exists at a high throttle for the component does not mean it can safely sustain this throttle for more than a few seconds. Go to the Tyto Robotics website to learn more about testing applications.
TA130-25 Kv80 Xoar47x10 T-motor U15 Kv80 Xoar40x10 test data
Author:
Uploaded by Erwan Labadie on 2019-04-09 19:06:16Tyto Robotics staff
Test equipment:
Series 1780Components:
Propulsion system 1
Motor:
Xoar TA130-25 KV80
Propeller:
Xoar PJP-T-L 47"x10"
ESC:
Xoar titan esc
Propulsion system 2
Motor:
T-Motor U15 V1
Propeller:
Xoar PJP-T-L 40"x10"
Plots
Plots
Propulsion system (powertrain) 1/2
ESC control protocol:
standard PWM 50 Hz
Derived data
Electrical power = Voltage × Current
Mechanical power = Torque × Rotation speed
Motor efficiency * = Mechanical power / Electrical power
Propeller efficiency = Thrust / Mechanical power
Powertrain efficiency = Thrust / Electrical power
* motor and ESC efficiencies are combined.
Derived data
Electrical power = Voltage × Current
Mechanical power = Torque × Rotation speed
Motor efficiency * = Mechanical power / Electrical power
Propeller efficiency = Thrust / Mechanical power
Powertrain efficiency = Thrust / Electrical power
* motor and ESC efficiencies are combined.
Propulsion system (powertrain) 2/2
ESC control protocol:
standard PWM 50 Hz
Combined multi rotors data
Combined multi rotors data
Combined thrust = Thrust A + Thrust B
Combined electrical power = Electrical power A + Electrical power B
Combined mechanical power = Mechanical power A + Mechanical power B
Combined motors efficiency = Combined mechanical power / Combined electrical power
Combined propellers efficiency = Combined thrust / Combined mechanical power
Combined overall efficiency = Combined thrust / Combined electrical power