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General

Field Elevation:
m SL
Temperature:
°C

Multicopter

# of Rotors:
Model Weight:
g
Framesize:
mm

Battery Cell

Cell Type (cont./max. C) - chrage state:
Configuration:
S
P
Discharge:

Controler

Type:

Motor              

Manufacturer - Motortype (Kv):
(Weight - g)
(² = discontinued)
Cooling:
Gear:
:1

Propeller

Type - yoke twist:
Diameter:
inch
Pitch:
inch
# Blades:
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Remarks:

Hover Time

Maximum

Temperatur

Thrust-Weight-Ratio

Battery

Load:
-
C
Voltage:
-
V
Rated Volrage:
-
V
Energy:
-
Wh
Capacity:
-
mAh
Used Capacitiy:
-
mAh
Hover Flight Time:
-
min

Motor @ Maximum

Total Current:
-
A
Voltage:
-
V
Revolution:
-
rpm
electric Power:
-
W
est. Temperature:
-
°C
-
°F
Thrust-Weight:
-
:1

Wattmeter & Logger readings

Current:
-
A
Voltage:
-
V
Power:
-
W

Motor @ Hover

Total Current:
-
A
Voltage:
-
V
Revolution:
-
rpm
Throttle (log):
-
%
Throttle (linear):
-
%
electric Power:
-
W
est. Temperature:
-
°C
-
°F
specific Thrust:
-
g/W
 
-
oz/W
Range Estimator

 
(c) copyright by and intellectual property of Markus Mueller, Solution for All, www.s4a.ch, info[at]ecalc.ch
See HTML Source for full and complete copyright notice.
Version: X / Data: with Motors