Battery
|
Cell Type
|
Number of cells
|
|
Cell Capacity
mAh
|
Cell Resistance
ohms
|
Cell Weight
oz = g
|
V per cell
volts
|
Pack Weight
oz = g
|
Pack Voltage
v
|
Speed Controller
|
|
Speed Controller Resistance
ohms
|
|
Motor
|
|
|
Kv
rpm/V
|
Kt
InOz/A
|
Rm
|
Io
A
|
Recommended Max Current
A
|
Weight
oz = g
|
Gearbox / Prop
|
Gear Ratio
|
Propeller
|
Prop Type
|
Prop Const
|
|
Prop Diameter
inches
|
Prop Pitch
inches
|
Prop Blades
|
Motor Results
|
Motor Amps
A
|
Volts to motor
V
|
Motor RPM
rpm
|
|
Watts In
W
|
Watts Out
W
|
Efficiency
%
|
Motor Max Efficiency
|
Current @ Max Eff
A
|
Volts to motor @ Max Eff
V
|
Watts In @ Max Eff
W
|
|
Watts Out @ Max Eff
W
|
Max Eff
%
|
Prop Results
|
Eff Diameter
inches
|
Prop RPM
rpm
|
Static Thrust
oz = kg
|
|
In-flight Thrust
oz = kg
|
Pitchspeed
mph = km/hod
|
Full-throttle duration minutes
|
Approx Power System Weight
oz = kg - Batteries + Motor + 10%
|
Dotaz
(Milan., 11. 4. 2012 20:57)