Drone Motors

1S tiny whoop motor

iFlight XING 1002

A 2.4 g motor for 1S tiny whoops: 19000KV or 22000KV, NSK bearings, and 53 g (19000KV) or 70 g (22000KV) of pull per motor on a 40 mm tri-blade on iFlight's 1S bench.

  • 1S tiny whoops
  • 40 mm tri-blade props
Drawing the 3D model…

The spin is an illustration: the model turns at 1/600 of the no-load speed, and it is a generic 1002 motor drawn from iFlight’s published sizes, not its exact design. Thrust, current and power are iFlight’s bench figures for the HQ 40 mm prop at 4 V, read straight across between its throttle steps. Its data starts at 50% throttle.

Version

iFlight tested it on 1S, at 4.1 V falling to 3.6 V at full throttle.

Max thrust
53 g
HQ 40 mm prop, 4 V
Weight
2.4 g
with wires; the same for both KVs
Peak current
5.3 A
full throttle
Max power
19 W
full throttle

from $13.99a motor at iFlight

A set of four: $55.96

Price seen Oct 19, 2026. Plain links: we earn nothing from them.

What it pulls

iFlight’s own bench test, one line per prop. Drag across the chart to move the throttle; the model above follows.

020406050%60%70%80%90%100%gthrottle53 gHQ 40 mm

At 60% with the HQ 40 mm: 34 g of thrust, 2.5 A, 10 W, 3.33 g per watt.

On your quad

0.3 : 1

Thrust to weight at full throttle: four motors pull 212 g with the HQ 40 mm at 4 V.

At 60% throttle they pull 136 g, 0.2 times the quad’s weight.

All-up weight is the quad ready to fly, with its battery and camera. The thrust is the maker’s static bench figure; in the air it is lower.

What you get for $13.99

What to pair it with

Our reading of iFlight’s numbers, so your build matches what the motor was tested with.

ESC
Rated for at least the peak iFlight measured at full throttle on a 40 mm tri-blade on 1S: 5.3 A for the 19000KV and 7.8 A for the 22000KV. (iFlight 19000KV test report, iFlight 22000KV test report)
Props
iFlight tested both KVs with an HQ 40 mm tri-blade: 25 g and 29 g at half throttle, 53 g and 70 g at full (19000KV and 22000KV). (iFlight 19000KV test report, iFlight 22000KV test report)
Battery
1S; iFlight gives 4 V as the input, and its bench runs fall from about 4.1 V at half throttle to 3.6 V at full. (iFlight product page, iFlight 19000KV test report, iFlight 22000KV test report)
Frame
Three M1.4 holes on a 6.6 mm circle. Four M1.4×4 screws come in the box. (iFlight product page, iFlight 19000KV test report)

Where to buy

  • iFlightthe maker's store; one motor, same price for both KVs
    $13.99seen Oct 19, 2026
    Visit

Plain links, not affiliate links. Prices change; the store’s page has the current one.

Full specs

SpecValueSource
KV19,000 rpm/V (also 22000KV)iFlight product page
Stator10 × 2 mm (1002)iFlight product page
Configuration9N12P (9 stator slots, 12 magnet poles)iFlight product page
Battery1S LiPo (4 V) (iFlight gives 4 V input for both KVs)iFlight product page
Weight2.4 g (with wires; the same for both KVs)iFlight product page
Dimensionsφ12.5 × 12.5 mm (from the shaft's end below the base to its tip); 9.25 mm to the top of the belliFlight 19000KV test report
Shaft1.5 mm, protrudes 3.25 mmiFlight product page
Mounting3 × M1.4 holes (φ1.4 mm) on a 6.6 mm circle; base plate 1 mm (iFlight's spec list says 3*3 φ1.4mm and its test report 3-φ1.4mm; its drawing dimensions the holes as 3-M1.4 on a φ6.6 circle)iFlight 19000KV test report
Bellsegmented (iFlight's term)iFlight product page
MagnetsN52H, curvediFlight product page
BearingsNSK φ4 × φ2 × 1.5 mmiFlight product page
Windingsingle-strand copperiFlight product page
Interphase resistance86 mΩ (70 mΩ for 22000KV)iFlight product page
Peak current5.3 A (100% throttle, HQ 40 mm tri-blade, 1S; 7.8 A for 22000KV)iFlight 19000KV test report
Max power19 W (28 W for 22000KV)iFlight 19000KV test report
Leads28 AWG, 50 mm, with an SH1.25 plugiFlight product page
In the box4 × M1.4×4 screwsiFlight product page

Bench data

Redrawn from iFlight’s test reports. Thrust is static pull on a bench, more than you get in flight. Power is volts × amps; efficiency is thrust divided by power.

19000KV on 1S, 4 V1 prop

PropThrottleVoltage (V)Current (A)Thrust (g)Power (W)Efficiency (g/W)
HQ 40 mm (three blades)motor at 57 °C50%4.131.52564.036
60%4.082.534103.333
70%3.963.441133.045
80%3.87446152.972
90%3.734.850182.793
100%3.625.353192.762

Source: iFlight 19000KV test report

22000KV on 1S, 4 V1 prop

PropThrottleVoltage (V)Current (A)Thrust (g)Power (W)Efficiency (g/W)
HQ 40 mm (three blades)motor at 60 °C50%4.111.92983.714
60%4.062.5536103.477
70%3.933.545143.272
80%3.844.2847162.86
90%3.75.1353192.792
100%3.617.870282.486

Source: iFlight 22000KV test report

Inside the motor

A brushless outrunner: the coils stand still in the middle and the magnets spin around them. From the top down:

How fast it spins

KV is the motor’s no-load speed per volt. With nothing on the shaft, the 19000KV version reaches about these speeds; a prop loads the motor and brings it down, typically to around 70–75% of these figures at full throttle.

BatteryVoltsNo-load rpm (KV × V)Electrical frequencyESC steps per second
4S nominal14.8281,20028,120 Hz168,720
4S full16.8319,20031,920 Hz191,520
6S nominal22.2421,80042,180 Hz253,080
6S full25.2478,80047,880 Hz287,280

A 12-pole rotor has 6 pole pairs, so every turn of the shaft is 6 electrical cycles, and a six-step ESC switches the phases 36 times per turn.

About the 3D model

A generic outrunner drawn from iFlight’s published sizes: the 10 × 2 mm stator, 12.5 mm bell, 1.5 mm shaft, 6.6 mm mounting circle and 9 teeth and 12 magnets. Anything iFlight doesn’t publish is typical for a motor this size, and the bell’s spoked top, the base and the inside are a generic design, not this motor’s. The colours are read off the maker’s product photos. There are no logos or markings: it is our drawing, not the maker’s.

Sources

  1. iFlight: XING 1002 FPV Motor (product page with a 19000KV/22000KV picker, and its product photos). Retrieved Oct 19, 2026.
  2. iFlight: XING 1002 19000KV test report (spec table, dimension drawing, thrust data). Retrieved Oct 19, 2026.
  3. iFlight: XING 1002 22000KV test report (spec table, dimension drawing, thrust data). Retrieved Oct 19, 2026.