eMotor Calculator
for Helicopter (Prototyp)
all Data without guarantee!
Accuracy +/-20%
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Design Fundamentals:            Field Elevation:
m.ü.M
   Air Temp:
°C
  Pressure (QNH):
hPa
Battery: (continuous / max. C)
   # seriell:
S
  # parallel:
P
  Capacity:
mAh
  Resistance:
Ohm
  Volt per Cell:
V
  Weight per Cell:
g
Contoller:
Resistance:
Ohm
Continuous Current:
A
max. Current:
A
Weight:
g
Motor: Manufacturer - Type (Kv in rpm/V)

  
Kv:
U/V
   Resistance:
Ohm
  Idle Current:
A
  Limit (up to 20s):
  Case length:
mm
  Weight:
g
Rotor:
Diameter:
cm
Pitch:
# Blades:
Rotor Const.:
 Gear Ratio:
Approx. Values:  Warning:    
Battery:    Load:
C
   Voltage:
V
   Rated Voltage:
V
Flight Time*:
min
mixed Flight Time:
min
Weight:
g
Motor: max. Strom:
A
Voltage:
V
Revolutions:
U/min
   el. Power (In):
W
   mech. Power (out):
W
   Efficiency:
%
Optimal Efficiency: Current:
A
Voltage:
V
Revolutions:
U/min
el. Power (In):
W
mech. Power (out):
W
Efficiency:
%
Rotor: Static Thrust:
g
Rotor Stall Thrust:
g
Revolutions:
U/min
Tip Speed:
km/h
Disc Load:
g/m2
Rotor Efficiency:
g/W
Entire Drive:   Weight:
g  (Batteriy + Contoller + Motor + 10%)
  P (in):
W
  P (out):
W
  Efficiency:
%

 Important Note:
 Before flight recheck the max. current! If your Current, el. Power or RPM are over the manufacturers limits your 
 motor, controller and/or battery may take damage!
Thrust reduction due long ducting are not considered!

 for printing use Landscape format
 * Flight Time @ Full Power
 ** Testdata with reduced accuracy

Motor Data:
Motor Cooling:
Power Scale:

Ampere