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.
DYS Samguk Wei HQ 5040 test data
Author:
Uploaded by Rob Hessler on 2019-03-20 06:13:47Test equipment:
RCbenchmark Series 1585Components:
Motor:
DYS Samguk Wei 2207 2600kv
Propeller:
HQ Prop 5040
Plots
Plots
Propulsion system (powertrain)
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.