Battery
| Load: |
- |
C |
| Voltage: |
- |
V |
| Rated Voltage: |
- |
V |
| 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 |
- |
% |
|
|
Motor @ Maximum
| Current: |
- |
A |
| Voltage: |
- |
V |
| Revolutions: |
- |
rpm |
| electric Power: |
- |
W |
| mech. Power: |
- |
W |
| Efficiency |
- |
% |
| est. Temperatur |
- |
°C |
| |
- |
°F |
|
|
Propeller
| Static Thrust: |
- |
g |
| |
- |
oz |
| Revolutions: |
- |
rpm |
| Stall Thrust: |
- |
g |
| |
- |
oz |
| Pitch Speed: |
- |
km/h |
| |
- |
mph |
| Tip Speed: |
- |
km/h |
| |
- |
mph |
| Efficiency |
- |
g/W |
| |
- |
oz/W |
|
|
Total Drive
| Drive Weight: |
- |
g |
| |
- |
oz |
| All Up Weight: |
- |
g |
| |
- |
oz |
| Power-Weight: |
- |
W/kg |
| |
- |
W/oz |
| Thrust-Weight: |
- |
:1 |
| P(in) @ max: |
- |
W |
| P(out) @ max: |
- |
W |
| Efficiency @ max: |
- |
% |
|