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Design Fundamentals:
 		Heli Weight:
 kg  		     Field Elevation:
m ASL		    Air Temp:
°C		   Pressure (QNH):
hPa
Battery: (continuous / max. C)
  		   # serial:
S 		  # parallel:
P 		  Capacity:
mAh		   Resistance:
Ohm		   Volt per Cell:
V		   Weight per Cell:
g
Controller:
 		Resistance:
Ohm 		Continuous Current:
A		 max. Current:
A		 Weight:
g		 Motor Weight:
g
Motor: Manufacturer - Type (Kv in rpm/V)
  		 Kv:
rpm/V 		   Resistance:
Ohm		   no-load Current:
A @ V		   Limit (up to 20s):
   # mag. Poles::
   Case length:
mm
Rotor: Bladetyp
 Diameter:
mm		 maximum Pitch:
 # Blades:
 Rotor Const.:
 Main Gear : Motor Pinion
: Teeth
Approx. Values:  Warning:    
Battery:    Load:
C		    Voltage:
V		    Rated Voltage:
V		 Flight Time max. Pitch:
min		 Flight Time Hover:
min		 Weight:
g
Motor at max. Pitch: max. Current:
A		 Voltage:
V		 Revolutions:
rpm		    el. Power (In):
W		    mech. Power (out):
W		    Efficiency:
%
Optimal Efficiency: Current:
A		 Voltage:
V		 Revolutions:
rpm		 el. Power (In):
W		 mech. Power (out):
W		 Efficiency:
%
Hover:
 Current:
A		 Voltage:
V		 Disc Load:
kg/m2 
oz/ft2		    el. Power (In):
W		    mech. Power (out):
W		    Efficiency:
%
Rotor: Static Thrust:
kg**
lbs**		 max. Governor*:
%		 max. Headspeed:
rpm		 Tip Speed:
km/h
mph		 max. forward speed:
km/h**
mph**		 Rotor Efficiency:
g/W**
oz/W**
Entire Drive:   Weight:
g   
(Battery + Contoller + Motor + 10%) 		 All up Weight:
kg		   P (in):
W		   P (out):
W		   Efficiency:
%
Motor Data:
 Motor Cooling:
 Power Scale:

Ampere

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
* Thrust Setting at Idle/Pitch 0°
 ** Testdata with reduced accuracy

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