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: |
- | | |