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T-Motor AT4130 KV450

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

19.12TWR
17.03EFTWR
7.80Thrust kg
0.408Weight kg
A$172.43Best 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
ModelAT4130
VariantKV450
KV450
Stator4130
Weight408 g
Max thrust7,800 g
Max current60.0 A
Max power2,500 W
Peak power3,117 W
No-load current1.40 A
Winding resistance0.060 Ω
Poles12
Max RPM10,572
Hover efficiency6.24 g/W
Peak-throttle efficiency2.50 g/W
Gradeprofessional
Applicationfixed-wing
Data confidencereported
Thrust basisreported
Efficiency basisreported
Measured test points11

Measured thrust curve

3,8947,787 3,117 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$172.43USD 119.99backorder48buy ↗
DrUAV CNA$234.06USD 162.88backorder48buy ↗
DrUAV CNA$241.35USD 167.95backorder48buy ↗

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

Thrust test points

PropellerCellsThrust gg/WBasis
unspecified—7,7872.50reported
unspecified—6,7512.80reported
unspecified—5,6943.37reported
unspecified—5,0803.75reported
unspecified—4,5694.66reported
unspecified—4,0104.91reported
unspecified—3,4845.22reported
unspecified—2,9285.70reported
unspecified—2,3426.24reported
unspecified—1,7797.01reported
unspecified—1,4317.39reported

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 →