Техническая Спецификация для Conrad Energy remote control ARF 2185 mm ROC006

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ROC006
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18. Technical Data
a) Flight Model 
Wing Span ............................................2185 mm
Length...................................................1248 mm
Wing area .............................................35.2 dm²
Area load ..............................................30.7 g/dm²
Weight incl. rechargeable battery .........1073 g
b) Motor and Propeller
Type ......................................................Brushless, 900 KV
Suitable for ...........................................3 LiPo cells
Propeller ...............................................30.48 x 15.24 cm (12“ x 6“)
c) Flight Controller
Voltage range .......................................2 - 4 cells LiPo
  Important!
 
The flight controller can be operated with 2 - 4 LiPo cells, but the flight model and the motor used is 
designed for only 3 LiPo cells. 
Current capacity ...................................Permanent current 35 A (for 10 seconds: 45 A)
BEC ......................................................linear, 5 V/DC, 4 A
Plug system ..........................................Banana plug/coupling 4 mm
d) Required Remote Control System (Not Enclosed) 
Transmission frequency........................2.4 GHz (recommended)
Number of channels .............................at least 5 (programmable computer remote control recommended from 6 
channels onwards)
Necessary mixer ...................................V-tail mixer
e) Required Flight Battery (Not Enclosed)
Battery type ..........................................3-cell LiPo battery, rated voltage 11.1 V, capacity min. 1200 mAh, discharge 
rate min. 25C