LUNN DYNAMICS

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T-Motor AT3520 KV550

professional uav brushless motor. Specs read from manufacturer page ↗.

19.80TWR
17.77EFTWR
4.32Thrust kg
0.218Weight kg
A$114.95Best price

advertised This thrust figure is the one the vendor advertises, read from their product copy. The throttle setting, propeller and cell count behind it are frequently unstated, so it is a guide rather than a measurement.

Compare in selector Buy from DrUAV

Specifications

BrandT-Motor
ModelAT3520
VariantKV550
KV550
Stator3520
Weight218 g
Max thrust4,316 g
Max current50.0 A
Max power1,100 W
Peak power1,098 W
No-load current1.10 A
Winding resistance0.031 Ω
Poles12
Max RPM9,014
Hover efficiency6.65 g/W
Peak-throttle efficiency3.93 g/W
Gradeprofessional
Applicationuav
Data confidencereported
Thrust basisreported
Efficiency basisreported
Measured test points11

Measured thrust curve

2,1584,316 1,098 W 0 W
Thrust (g) against electrical input power (W), 11 measured points from the manufacturer's test table.

Where to buy

VendorPriceAs listedStockLead days
DrUAV CNA$114.95USD 79.99backorder48buy ↗
DrUAV CNA$114.95USD 79.99backorder48buy ↗
DrUAV CNA$175.32USD 122.00backorder48buy ↗

Multi-pack listings are shown at their per-unit price so they stay comparable.

Thrust test points

PropellerCellsThrust gg/WBasis
unspecified—4,3163.93reported
unspecified—4,0724.14reported
unspecified—3,4574.58reported
unspecified—3,1014.87reported
unspecified—2,8175.17reported
unspecified—2,5265.47reported
unspecified—2,1855.84reported
unspecified—1,8816.22reported
unspecified—1,5836.65reported
unspecified—1,3327.24reported
unspecified—1,0767.72reported

Compatible accessories

Parts this catalogue holds that fit this component, and the evidence behind each pairing. Fit is inferred from published specifications, not from having tried it. Confirm mounting and clearance before you buy.

rule of thumb The size conventionally run on a stator this big. Not a measurement -- check clearance and current draw before flying it.

CAD model

No CAD model linked yet.

How the metrics are calculated

TWR is max thrust divided by motor weight, motor only, static, excluding propeller and ESC. EFTWR scales that by hover efficiency and RPM headroom, so it equals TWR for a motor at 8 g/W and 10,000 RPM. Full methodology and the whole catalogue →