LUNN DYNAMICS

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T-Motor AT3530 KV580

professional fixed-wing brushless motor. Specs read from manufacturer page ↗.

16.11TWR
14.40EFTWR
4.80Thrust kg
0.298Weight kg
A$143.69Best 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
ModelAT3530
VariantKV580
KV580
Stator3530
Weight298 g
Max thrust4,800 g
Max current65.0 A
Max power1,400 W
Peak power1,263 W
No-load current1.90 A
Winding resistance0.018 Ω
Poles12
Max RPM9,496
Hover efficiency6.49 g/W
Peak-throttle efficiency3.80 g/W
Gradeprofessional
Applicationfixed-wing
Data confidencereported
Thrust basisreported
Efficiency basismeasured
Measured test points12

Measured thrust curve

2,4024,805 1,263 W 0 W
Thrust (g) against electrical input power (W), 12 measured points from the manufacturer's test table.

Where to buy

VendorPriceAs listedStockLead days
DrUAV CNA$143.69USD 99.99backorder48buy ↗
DrUAV CNA$143.69USD 99.99backorder48buy ↗

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

Thrust test points

PropellerCellsThrust gg/WBasis
unspecified—4,8053.80measured
unspecified—4,6604.17measured
unspecified—4,2654.42measured
unspecified—3,8264.69measured
unspecified—3,4504.90measured
unspecified—3,1045.13measured
unspecified—2,7365.45measured
unspecified—2,3695.80measured
unspecified—2,0636.16measured
unspecified—1,7956.49measured
unspecified—1,5816.85measured
unspecified—1,3827.11measured

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 →