| Cobra C-5320-18 370Kv Motor Propeller Data | |||||||||||||||
| Magnets | Motor Wind | Motor Kv | No-Load Current | Motor Resistance | I Max | P Max (8S) | |||||||||
| 14-Pole | 18-Turn Delta | 370 RPM/Volt | Io = 2.50 Amps @ 20v | Rm = 0.023 Ohms | 75 Amps | 2220 W | |||||||||
| Stator | Outside Diameter | Body Length | Total Shaft Length | Shaft Diameter | Motor Weight | ||||||||||
| 12-Slot | 63.0 mm, 2.48 in. | 50.5 mm, 1.99 in. | 84.3 mm, 3.32 in. | 8.00 mm, 0.315 in. | 490 grams, 17.28 oz. | ||||||||||
| Test Data From | Input | 16.0 V | 20.0 V | 24.0V | 28.0V | Measured Kv value | Measured Rm Value | ||||||||
| Sample Motor | Io Value | 2.157 A | 2.495 A | 2.883 A | 3.497 A | 369.6 RPM/Volt @ 20V | 0.0227 Ohms | ||||||||
| Prop | Prop | Li-Po | Input | Motor | Input | Prop | Pitch Speed | Thrust | Thrust | Thrust Eff. | |||||
| Manf. | Size | Cells | Voltage | Amps | Watts | RPM | in MPH | Grams | Ounces | Grams/W | |||||
| APC | 15x6-E | 6 | 22.2 | 26.54 | 589.3 | 7,406 | 42.1 | 3,208 | 113.16 | 5.44 | |||||
| APC | 15x8-E | 6 | 22.2 | 29.91 | 664.0 | 7,398 | 56.0 | 3,297 | 116.30 | 4.97 | |||||
| APC | 15x10-E | 6 | 22.2 | 43.99 | 976.6 | 7,085 | 67.1 | 3,703 | 130.62 | 3.79 | |||||
| APC | 16x8-E | 6 | 22.2 | 36.45 | 809.1 | 7,277 | 55.1 | 3,767 | 132.88 | 4.66 | |||||
| APC | 16x10-E | 6 | 22.2 | 53.05 | 1177.7 | 6,905 | 65.4 | 4,403 | 155.31 | 3.74 | |||||
| APC | 16x12-E | 6 | 22.2 | 62.97 | 1397.9 | 6,724 | 76.4 | 3,959 | 139.65 | 2.83 | |||||
| APC | 17x8-E | 6 | 22.2 | 52.02 | 1154.8 | 6,950 | 52.7 | 4,907 | 173.09 | 4.25 | |||||
| APC | 17x10-E | 6 | 22.2 | 62.14 | 1379.5 | 6,738 | 63.8 | 5,078 | 179.12 | 3.68 | |||||
| APC | 17x12-E | 6 | 22.2 | 69.59 | 1544.8 | 6,580 | 74.8 | 4,956 | 174.82 | 3.21 | |||||
| APC | 18x8-E | 6 | 22.2 | 52.62 | 1168.3 | 6,934 | 52.5 | 5,778 | 203.81 | 4.95 | |||||
| APC | 18x10-E | 6 | 22.2 | 63.51 | 1409.9 | 6,687 | 63.3 | 6,038 | 212.98 | 4.28 | |||||
| APC | 18x12-E | 6 | 22.2 | 87.31 | 1938.4 | 6,523 | 74.1 | 5,622 | 198.31 | 2.90 | |||||
| APC | 19x8-E | 6 | 22.2 | 74.60 | 1656.1 | 6,527 | 49.4 | 6,766 | 238.66 | 4.09 | |||||
| APC | 19x10-E | 6 | 22.2 | 72.43 | 1607.9 | 6,538 | 61.9 | 6,908 | 243.67 | 4.30 | |||||
| APC | 19x12-E | 6 | 22.2 | 86.20 | 1913.6 | 6,515 | 74.0 | 7,017 | 247.51 | 3.67 | |||||
| APC | 20x8-E | 6 | 22.2 | 76.45 | 1697.2 | 6,562 | 49.7 | 7,580 | 267.37 | 4.47 | |||||
| Prop | Prop | Li-Po | Input | Motor | Input | Prop | Pitch Speed | Thrust | Thrust | Thrust Eff. | |||||
| Manf. | Size | Cells | Voltage | Amps | Watts | RPM | in MPH | Grams | Ounces | Grams/W | |||||
| APC | 15x6-E | 7 | 25.9 | 37.08 | 960.2 | 8,500 | 48.3 | 4,366 | 154.00 | 4.55 | |||||
| APC | 15x8-E | 7 | 25.9 | 40.59 | 1051.4 | 8,413 | 63.7 | 4,304 | 151.82 | 4.09 | |||||
| APC | 15x10-E | 7 | 25.9 | 60.84 | 1575.8 | 7,990 | 75.7 | 4,690 | 165.43 | 2.98 | |||||
| APC | 16x8-E | 7 | 25.9 | 66.78 | 1729.7 | 7,889 | 59.8 | 5,489 | 193.62 | 3.17 | |||||
| APC | 16x10-E | 7 | 25.9 | 73.47 | 1902.8 | 7,787 | 73.7 | 5,558 | 196.05 | 2.92 | |||||
| APC | 16x12-E | 7 | 25.9 | 83.78 | 2169.9 | 7,686 | 87.3 | 5,012 | 176.79 | 2.31 | |||||
| APC | 17x8-E | 7 | 25.9 | 70.75 | 1832.5 | 7,873 | 59.6 | 6,219 | 219.37 | 3.39 | |||||
| APC | 17x10-E | 7 | 25.9 | 84.51 | 2188.9 | 7,633 | 72.3 | 6,436 | 227.02 | 2.94 | |||||
| APC | 18x8-E | 7 | 25.9 | 69.42 | 1798.1 | 7,850 | 59.5 | 7,415 | 261.55 | 4.12 | |||||
| APC | 18x10-E | 7 | 25.9 | 83.79 | 2170.1 | 7,650 | 72.4 | 7,749 | 273.34 | 3.57 | |||||
| Prop | Prop | Li-Po | Input | Motor | Input | Prop | Pitch Speed | Thrust | Thrust | Thrust Eff. | |||||
| Manf. | Size | Cells | Voltage | Amps | Watts | RPM | in MPH | Grams | Ounces | Grams/W | |||||
| APC | 15x6-E | 8 | 29.6 | 49.72 | 1471.6 | 9,445 | 53.7 | 5,381 | 189.81 | 3.66 | |||||
| APC | 15x8-E | 8 | 29.6 | 53.14 | 1572.9 | 9,384 | 71.1 | 5,307 | 187.20 | 3.37 | |||||
| APC | 15x10-E | 8 | 29.6 | 81.15 | 2402.0 | 9,027 | 85.5 | 5,647 | 199.19 | 2.35 | |||||
| Propeller Chart Color Code Explanation | |||||||||||||||
| The prop is to small to get good performance from the motor. (Less than 50% power) | |||||||||||||||
| The prop is sized right to get good power from the motor. (50 to 80% power) | |||||||||||||||
| The prop can be used, but full throttle should be kept to short bursts. (80 to 100% power) | |||||||||||||||
| The prop is too big for the motor and should not be used. (Over 100% power) | |||||||||||||||
| PLEASE NOTE: | |||||||||||||||
| The Data contained in this Prop Chart is based on actual measurements, taken in a controlled test environment, at an altitude of | |||||||||||||||
| 584 feet above sea level. The test voltages used are based on the standard output of a Li-Po battery under load, which is 3.70 volts | |||||||||||||||
| per cell. If you are using a battery that is larger in capacity than normal, or has a very high C-rating, then your actual voltages will | |||||||||||||||
| be higher than those shown in the chart, and this will result in a higher current and power value for every prop used. You should | |||||||||||||||
| always test your actual power system with a watt meter before flying your model to make sure that you are not exceeding the | |||||||||||||||
| recommended current and power ratings of the motor being used. The prop recommendations in this chart assume that the motor | |||||||||||||||
| receives adequate cooling throughout its operation. If your motor is being used inside a cowl or fuselage, you must ensure that | |||||||||||||||
| the motor receives sufficient airflow, and does not get too hot during operation. It is always best to use a prop size that pulls no | |||||||||||||||
| more than 80% of the motors maximum recommended current value to ensure safe operation under all conditions. | |||||||||||||||