Formula:
Key Formulas for Drone Propulsion:
1. Required Thrust per Motor:
Tmotor (g) = (Wdrone (g) × TWR) ÷ Nmotors
2. Estimated Propeller RPM:
RPM = Kv (RPM/V) × Vbatt (V) × ηmotor
Where:
- Tmotor: Required Thrust per Motor (grams)
- Wdrone: Total Drone Weight (grams)
- TWR: Desired Thrust-to-Weight Ratio (e.g., 2 for stable, 5 for acrobatic)
- Nmotors: Number of Motors on the drone
- Kv: Motor Kv rating (RPM per Volt)
- Vbatt: Nominal Battery Voltage (Volts)
- ηmotor: Motor Efficiency Factor (decimal, e.g., 0.85)
Note: Current and Power estimations are simplified for guidance. Always refer to specific motor/propeller datasheets for precise performance.