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Scorpion A-5524-205kv V2

By Scorpion ↗

The Scorpion A-5524-205kv V2 is a 205 RPM/Volt BLDC propulsion motor for acrobatic and sport/UAV airplanes. Supplied with mounting and connection accessories, it has a 74.0mm x 65.8mm body and a 12s LiPo rating. Continuous power is 3552 Watts, with higher output limited to intermittent operation.

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Scorpion A-5524-205kv V2 motor in black and gold, shown from two angles
Scorpion A-5524-205kv V2 motor in black and gold, shown from two angles
Product identityScorpion A-5524-205kv V2
Intended applicationsMotor for 74"-78" acrobatic airplanes or sport/UAV airplanes requiring up to 5000w on a 12s battery.12s battery.
Motor Kv205 RPM / Volt
Motor weight622g (21.94 oz)Motor only.
Weight with prop mount accessories655g (23.01 oz)Including prop mount accessories.
Motor body dimensions74.0 mm x 65.8mm (2.93" x 2.60")

Product overview

The Scorpion A-5524-205kv V2 serves 74"–78" acrobatic airplanes and sport/UAV aircraft, with a stated single-engine sport/UAV aircraft weight range of 30–40kg. Its BLDC architecture combines a 55.0mm-diameter, 24mm-thick stator with 12 stator arms, 14 magnet poles and a 9T/10T Delta winding. Silicon steel stator sheets are 0.2mm thick, while the enamel-coated copper windings use two 0.96mm strands rated above 200C+. For installation planning, the motor body measures 74.0mm x 65.8mm, the external shaft is 10mm, and weight rises from 622g for the motor alone to 655g with prop mount accessories.

The supplied configuration contains the motor, an A-55/65 cross mount, four M4 mounting bolts, three prop bore spacers, three female 6mm connectors, three heat-shrink pieces, three stickers and two M8 nuts. Recommended integration choices are 21x12, 22x10E or 23x8E propellers and a Tribunus III 14-150A ESC SBEC. Continuous ratings are 80A and 3552 Watts; peak ratings reach 105A and 4662 Watts for intermittent full-throttle use lasting 5–60 seconds, depending on application and cooling. The maximum rated LiPo configuration is 12s, with higher cell counts possible when using smaller propellers.

Specifications

SpecificationValue & conditions
Product identityScorpion A-5524-205kv V2
Intended applicationsMotor for 74"-78" acrobatic airplanes or sport/UAV airplanes requiring up to 5000w on a 12s battery.12s battery.
Motor Kv205 RPM / Volt
Motor weight622g (21.94 oz)Motor only.
Weight with prop mount accessories655g (23.01 oz)Including prop mount accessories.
Motor body dimensions74.0 mm x 65.8mm (2.93" x 2.60")
External shaft diameter10mm
Continuous current80AContinuous operation.
Continuous power3552 WattsContinuous operation.
Peak current105AIntermittent full throttle usage ranging from 5 - 60 seconds depending on use case and cooling.
Peak power4662 WattsIntermittent full throttle usage ranging from 5 - 60 seconds depending on use case and cooling.
Maximum rated LiPo cell count12sHigher cell count possible with smaller prop usage.
Stator diameter55.0 mm (2.16 in)
Stator thickness24 mm (.95 in)
Number of stator arms12
Magnet poles14
Motor winding9T/10T Delta
Motor wire2-Strand x 0.96mm
No-load current1.51 AmpsIO/20V.
Motor internal resistance35 mΩPhase-phase.
Motor inductance40µHPhase-phase at 1khz.
Recommended ESCTribunus III 14-150A ESC SBEC
Acrobatic aircraft weight range6.2kg - 9.3kg (13.6lbs - 20.5lbs)Acrobatic airplane application.
Sport / UAV aircraft weight range30kg - 40kg (66lbs -88lbs)Sport / UAV, single engine.
Recommended propellers21x12 / 22x10E / 23x8E
Stator sheets and winding construction0.2mm silicon steel stator sheets; 2 x single-strand 0.96mm enamel-coated copper wire windings rated above 200C+.
Included equipment1 x Scorpion A-5524 BLDC Motor; 1 x A-55/65 Cross Mount (stock); 4 x M4 Cross Mount Mounting Bolts; 3 x Prop Bore Spacers (8x10x 4/4/10); 3 x Female 6mm Connectors; 3 x Heat Shrink; 3 x Scorpion Stickers; 2 x M8 Nuts.Supplied box configuration.
Peak operation duration5 - 60 secondsIntermittent full throttle; duration depends on use case and cooling.
Higher cell count provisionHigher cell count possible with smaller prop usage.Smaller prop usage.
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