Техническая Спецификация для Reely remote control RtF 2100 mm 1289571
Модели
1289571
53
15. Declaration of Conformity (DOC)
The manufacturer hereby declares that this product complies with the essential requirements and regulations and all
other relevant provisions of the 1999/5/EC directive.
The compliance statement for this product is available at www.conrad.com.
16. Technical Data
Model:
Wing Span ........................................................... 2100 mm
Length.................................................................. 1170 mm
Weight ................................................................ Ready to fly from approx. 1220 g upwards
Control ................................................................. 4 channels (aileron, elevator, rudder, motor)
Propeller .............................................................. 22.8 x 17.8 cm (9“ x 7“)
Length.................................................................. 1170 mm
Weight ................................................................ Ready to fly from approx. 1220 g upwards
Control ................................................................. 4 channels (aileron, elevator, rudder, motor)
Propeller .............................................................. 22.8 x 17.8 cm (9“ x 7“)
Electric Engine:
Power consumption ............................................. max. approx. 240 W
Operating voltage ................................................ 2 - 3 cell LiPo (7,4 - 11.1 V)
Current capacity .................................................. Permanent current 18 A
Revolutions per Volt ............................................. 1000 KV
Operating voltage ................................................ 2 - 3 cell LiPo (7,4 - 11.1 V)
Current capacity .................................................. Permanent current 18 A
Revolutions per Volt ............................................. 1000 KV
Flight Controller:
Input voltage ........................................................ 2 - 3 cells LiPo (7.4 - 11.1 V)
Current capacity .................................................. Permanent current 25 A, short term (5 s) max. 35 A
Undervoltage recognition ..................................... LiPo 3.0 V/cell, LiFe 2.5 V/cell, NiMH 0.8 V/cell
BEC-output (linear) .............................................. 5 V/DC, 1,5 A
Current capacity .................................................. Permanent current 25 A, short term (5 s) max. 35 A
Undervoltage recognition ..................................... LiPo 3.0 V/cell, LiFe 2.5 V/cell, NiMH 0.8 V/cell
BEC-output (linear) .............................................. 5 V/DC, 1,5 A
Flight Battery:
Battery technology ............................................... LiPo
Number of cells .................................................... 3 (rated voltage 11.1 V)
Capacity ............................................................... 1500 mAh
Discharge rate ..................................................... 12 C
Number of cells .................................................... 3 (rated voltage 11.1 V)
Capacity ............................................................... 1500 mAh
Discharge rate ..................................................... 12 C