LUNN DYNAMICS

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T-Motor MN2806 KV650

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

24.44TWR
26.45EFTWR
1.10Thrust kg
0.045Weight kg
A$71.71Best 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
ModelMN2806
VariantKV650
KV650
Stator2806
Weight45 g
Max thrust1,100 g
Max current16.0 A
Max power160 W
Peak power186 W
No-load current0.45 A
Winding resistance0.201 Ω
Poles12
Max RPM6,061
Hover efficiency10.89 g/W
Peak-throttle efficiency6.10 g/W
Gradeprofessional
Applicationuav
Data confidencereported
Thrust basisreported
Efficiency basisreported
Measured test points13

Measured thrust curve

5691,138 186 W 0 W
Thrust (g) against electrical input power (W), 13 measured points from the manufacturer's test table.

Where to buy

VendorPriceAs listedStockLead days
DrUAV CNA$71.71USD 49.90backorder48buy ↗
DrUAV CNA$106.50USD 74.11backorder48buy ↗

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

Thrust test points

PropellerCellsThrust gg/WBasis
unspecified—1,1386.10reported
unspecified—1,0906.35reported
unspecified—1,0156.66reported
unspecified—9417.04reported
unspecified—8637.44reported
unspecified—7857.90reported
unspecified—7008.36reported
unspecified—6268.78reported
unspecified—5579.34reported
unspecified—48510.06reported
unspecified—41710.89reported
unspecified—34611.87reported
unspecified—26913.16reported

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 →