Battery
| Load: |
- |
C |
| Voltage: |
- |
V |
| Rated Voltage: |
- |
V |
| Energy: |
- |
Wh |
| Capacity: |
- |
mAh |
| Capacity used: |
- |
mAh |
| min. Flight Time: |
- |
min |
| Mixed Flight
Time: |
- |
min |
| Weight: |
- |
g |
| |
- |
oz |
|
|
Motor @ Optimum
Efficiency
| Current: |
- |
A |
| Voltage: |
- |
V |
| Revolutions: |
- |
rpm |
| electric Power: |
- |
W |
| mech. Power: |
- |
W |
| Efficiency |
- |
% |
| |
|
|
| |
|
|
| |
|
|
| |
|
|
Wattmeter & Logger readings
| Current: |
- |
A |
| Voltage: |
- |
V |
| Power: |
- |
W |
|
|
Motor @ Maximum
| Current: |
- |
A |
| Voltage: |
- |
V |
| Revolutions: |
- |
rpm |
| electric Power: |
- |
W |
| mech. Power: |
- |
W |
| Efficiency: |
- |
% |
| est. Temperatur: |
- |
°C |
| |
- |
°F |
| Rm: |
- |
mΩ |
| Controller: |
- |
epm |
Thermal Curve
| - |
- |
- |
- |
s |
| - |
- |
- |
- |
°C |
| - |
- |
- |
- |
°F |
|
|
Propeller
| Static Thrust: |
- |
g |
| |
- |
oz |
| Revolutions: |
- |
rpm |
| Stall Thrust: |
- |
g |
| |
- |
oz |
| Thrust @ Speed: |
- |
g |
| Thrust @ Speed: |
- |
oz |
| Pitch Speed: |
- |
km/h |
| |
- |
mph |
| Tip Speed: |
- |
km/h |
| |
- |
mph |
| specific Thrust |
- |
g/W |
| |
- |
oz/W |
| n100W: |
- |
rpm |
| n10N: |
- |
rpm |
|
|
Total Drive
| Drive Weight: |
- |
g |
| |
- |
oz |
| Power-Weight: |
- |
W/kg |
| |
- |
W/oz |
| Thrust-Weight: |
- |
:1 |
| Current @ max: |
- |
A |
| P(in) @ max: |
- |
W |
| P(out) @ max: |
- |
W |
| Efficiency @
max: |
- |
% |
| Torque: |
- |
Nm |
| |
- |
lbf.ft |
| Climb Capacity: |
- |
m |
| |
- |
ft |
|
|
Model
| All Up Weight: |
- |
g |
| |
- |
oz |
| Wing Load: |
- |
g/dm² |
| |
- |
oz/ft² |
| Cubic Wing Load: |
- |
|
| est. Stall Speed: |
- |
km/h |
| |
- |
mph |
| max. Speed (level): |
- |
km/h |
| |
- |
mph |
| max. Speed
(vertical): |
- |
km/h |
| |
- |
mph |
| max. rate of climb: |
- |
m/s |
| ( ~-...-° ) |
- |
ft/min |
|