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General   Model Weight:
 g  
 oz 		  # of Rotors:

   Frame Size:
 mm
 inch		   FCU Tilt limit:

       Field Elevation:
 m ASL
 ft ASL 		  Air Temperature:
 °C
 °F		   Pressure (QNH):
 hPa
 inHg
Battery Cell   Type (Cont. / max. C) - charge state:
- 		  Configuration:
 S     P		   Cell Capacity:
 mAh
 mAh total
   max. discharge:
   Resistance:
 Ohm		   Voltage:
 V		   C-Rate:
 C cont.
 C max.		   Weight:
 g
 oz
Controller   Type:
   Current:
 A cont.
 A max.		   Resistance:
 Ohm		   Weight:
 g
 oz		       Accessories   Current drain:
 A		   Weight:
 g
 oz
Motor   Manufacturer - Type (Kv) - Cooling:  (² = discontinued)
 - 
  Kv (w/o torque):
 rpm/V
   no-load current:
 A @ V		   Limit (up to 15s):
   Resistance:
 Ohm		   Case length:
 mm
 inch		   # mag. Poles:
   Weight:
 g
 oz
Propeller   Type - yoke twist:
- 		  Diameter:
 inch
 mm 		  Pitch:
 inch
 mm 		  # Blades:
   PConst/TConst:
/ 		  Gear Ratio:
 : 1		        

Load

Hover Time

Maximum

Temperatur

Thrust-Weight-Ratio

spec. Thrust

Configuration
Remarks:    
Battery
Load: - C
Voltage: - V
Rated Voltage: - V
Energy: - Wh
Capacity: - mAh
Capacity used: - mAh
min. Flight Time: - min
Mixed Flight Time: - min
Hover Flight Time: - min
Weight: - g
  - oz
  Motor @ Optimum Efficiency
Current: - A
Voltage: - V
Revolutions: - rpm
electric Power: - W
mech. Power: - W
Efficiency - %
  Motor @ Maximum
Current: - A
Voltage: - V
Revolutions: - rpm
electric Power: - W
mech. Power: - W
Power-Weight: - W/kg
  - W/oz
Efficiency - %
est. Temperatur - °C
  - °F
 
Wattmeter & Logger readings
Current: - A
Voltage: - V
Power: - W
  Motor @ Hover
Current: - A
Voltage: - V
Revolutions: - rpm
Throttle (log): - %
Throttle (linear): - %
electric Power: - W
mech. Power: - W
Power-Weight: - W/kg
  - W/oz
Efficiency - %
est. Temperatur - °C
  - °F
specific Thrust - g/W
  - oz/W
  Total Drive
Drive Weight: - g
  - oz
Thrust-Weight: - :1
Current @ hover: - A
P(in) @ Hover: - W
P(out) @ Hover: - W
Efficiency @ Hover: - %
Current @ max: - A
P(in) @ max: - W
P(out) @ max: - W
Efficiency @ max: - %
  Multicopter
All Up Weight: - g
  - oz
add Payload: - g
  - oz
max. Tilt: - °
max. Speed: - km/h
  - mph
est. Range - m
  - mi
max. rate of climb: - m/s
  - ft/min
Total Disc Area: - dm²
- in²
Engine failure: -
Range Estimator

Speed (km/h)
Motor Characteristics
Ampere
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Version: X / Data: with Motors