| Cobra C-5330-22 205Kv Motor Propeller Data | |||||||||||||||
| Magnets | Motor Wind | Motor Kv | No-Load Current | Motor Resistance | I Max | P Max (12S) | |||||||||
| 14-Pole | 22-Turn Delta | 205 RPM/Volt | Io = 1.55 Amps @ 20v | Rm = 0.034 Ohms | 55 Amps | 2440 W | |||||||||
| Stator | Outside Diameter | Body Length | Total Shaft Length | Shaft Diameter | Motor Weight | ||||||||||
| 12-Slot | 63.0 mm, 2.48 in. | 60.5 mm, 2.38 in. | 94.3 mm, 3.71 in. | 8.00 mm, 0.315 in. | 649 grams, 22.89 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 | 1.422 A | 1.545 A | 1.682 A | 1.811 A | 212.5 RPM/Volt @ 20V | 0.0337 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 | 15x10-E | 10 | 37.0 | 26.23 | 970.6 | 7,034 | 66.6 | 3,668 | 129.38 | 3.78 | |||||
| APC | 16x8-E | 10 | 37.0 | 27.38 | 1013.1 | 6,871 | 52.1 | 4,259 | 150.23 | 4.20 | |||||
| APC | 16x10-E | 10 | 37.0 | 31.59 | 1168.9 | 6,900 | 65.3 | 4,444 | 156.76 | 3.80 | |||||
| APC | 16x12-E | 10 | 37.0 | 37.65 | 1393.2 | 6,784 | 77.1 | 4,088 | 144.20 | 2.93 | |||||
| APC | 17x8-E | 10 | 37.0 | 30.98 | 1146.2 | 6,916 | 52.4 | 5,008 | 176.65 | 4.37 | |||||
| APC | 17x10-E | 10 | 37.0 | 37.51 | 1387.8 | 6,783 | 64.2 | 5,275 | 186.07 | 3.80 | |||||
| APC | 17x12-E | 10 | 37.0 | 42.09 | 1557.5 | 6,692 | 76.0 | 5,193 | 183.18 | 3.33 | |||||
| APC | 18x8-E | 10 | 37.0 | 30.82 | 1140.3 | 6,913 | 52.4 | 5,892 | 207.83 | 5.17 | |||||
| APC | 18x10-E | 10 | 37.0 | 37.77 | 1397.3 | 6,773 | 64.1 | 6,140 | 216.58 | 4.39 | |||||
| APC | 18x12-E | 10 | 37.0 | 54.07 | 2000.6 | 6,481 | 73.6 | 6,099 | 215.13 | 3.05 | |||||
| APC | 19x8-E | 10 | 37.0 | 46.34 | 1714.5 | 6,617 | 50.1 | 7,142 | 251.92 | 4.17 | |||||
| APC | 19x10-E | 10 | 37.0 | 43.99 | 1627.5 | 6,658 | 63.0 | 7,238 | 255.31 | 4.45 | |||||
| APC | 19x12-E | 10 | 37.0 | 52.48 | 1941.8 | 6,500 | 73.9 | 7,482 | 263.92 | 3.85 | |||||
| APC | 20x8-E | 10 | 37.0 | 46.52 | 1721.2 | 6,600 | 50.0 | 7,943 | 280.18 | 4.61 | |||||
| APC | 20x10-E | 10 | 37.0 | 55.48 | 2052.8 | 6,441 | 61.0 | 8,438 | 297.64 | 4.11 | |||||
| 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 | 15x8-E | 12 | 44.4 | 23.15 | 1027.9 | 8,329 | 63.1 | 4,266 | 150.48 | 4.15 | |||||
| APC | 15x10-E | 12 | 44.4 | 38.34 | 1702.4 | 8,133 | 77.0 | 4,904 | 172.98 | 2.88 | |||||
| APC | 16x8-E | 12 | 44.4 | 42.46 | 1885.4 | 8,045 | 60.9 | 5,870 | 207.06 | 3.11 | |||||
| APC | 16x10-E | 12 | 44.4 | 46.08 | 2046.1 | 7,961 | 75.4 | 5,929 | 209.14 | 2.90 | |||||
| APC | 16x12-E | 12 | 44.4 | 51.59 | 2290.7 | 7,836 | 89.0 | 5,458 | 192.52 | 2.38 | |||||
| APC | 17x8-E | 12 | 44.4 | 44.15 | 1960.0 | 8,000 | 60.6 | 6,628 | 233.79 | 3.38 | |||||
| APC | 17x10-E | 12 | 44.4 | 53.26 | 2364.5 | 7,800 | 73.9 | 7,065 | 249.21 | 2.99 | |||||
| APC | 17x12-E | 12 | 44.4 | 59.07 | 2622.8 | 7,694 | 87.4 | 6,877 | 242.58 | 2.62 | |||||
| APC | 18x8-E | 12 | 44.4 | 43.00 | 1909.0 | 8,029 | 60.8 | 8,059 | 284.27 | 4.22 | |||||
| APC | 18x10-E | 12 | 44.4 | 50.05 | 2222.2 | 7,722 | 73.1 | 8,032 | 283.32 | 3.61 | |||||
| APC | 19x8-E | 12 | 44.4 | 65.51 | 2908.6 | 7,571 | 57.4 | 9,164 | 323.25 | 3.15 | |||||
| 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. | |||||||||||||||