| Cobra C-5340-16 200Kv Motor Propeller Data | |||||||||||||||
| Magnets | Motor Wind | Motor Kv | No-Load Current | Motor Resistance | I Max | P Max (12S) | |||||||||
| 14-Pole | 16-Turn Delta | 200 RPM/Volt | Io = 3.05 Amps @ 40v | Rm = 0.025 Ohms | 64 Amps | 2840 W | |||||||||
| Stator | Outside Diameter | Body Length | Total Shaft Length | Shaft Diameter | Motor Weight | ||||||||||
| 12-Slot | 63.0 mm, 2.48 in. | 71.0 mm, 2.80 in. | 102.4 mm, 4.03 in. | 8.00 mm, 0.315 in. | 804 grams, 28.36 oz. | ||||||||||
| Test Data From | Input | 28.0 V | 32.0 V | 36.0V | 40.0V | Measured Kv value | Measured Rm Value | ||||||||
| Sample Motor | Io Value | 2.44 A | 2.62 A | 2.99 A | 3.05 A | 205 RPM/Volt @ 40V | 0.025 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 | 16x8-E | 10 | 37.0 | 30.49 | 1128.2 | 7,083 | 53.7 | 4,573 | 161.31 | 4.05 | |||||
| APC | 16x10-E | 10 | 37.0 | 34.46 | 1275.2 | 7,009 | 66.4 | 4,631 | 163.35 | 3.63 | |||||
| APC | 16x12-E | 10 | 37.0 | 40.98 | 1516.1 | 6,880 | 78.2 | 4,294 | 151.46 | 2.83 | |||||
| APC | 17x8-E | 10 | 37.0 | 33.28 | 1231.3 | 7,046 | 53.4 | 5,355 | 188.89 | 4.35 | |||||
| APC | 17x10-E | 10 | 37.0 | 40.40 | 1494.7 | 6,926 | 65.6 | 5,673 | 200.11 | 3.80 | |||||
| APC | 17x12-E | 10 | 37.0 | 46.20 | 1709.5 | 6,826 | 77.6 | 5,640 | 198.94 | 3.30 | |||||
| APC | 18x8-E | 10 | 37.0 | 32.58 | 1205.3 | 6,932 | 52.5 | 6,151 | 216.97 | 5.10 | |||||
| APC | 18x10-E | 10 | 37.0 | 38.66 | 1430.6 | 6,780 | 64.2 | 6,357 | 224.23 | 4.44 | |||||
| APC | 18x12-E | 10 | 37.0 | 58.18 | 2152.5 | 6,631 | 75.4 | 6,714 | 236.83 | 3.12 | |||||
| APC | 19x8-E | 10 | 37.0 | 47.15 | 1744.7 | 6,666 | 50.5 | 7,373 | 260.07 | 4.23 | |||||
| APC | 19x10-E | 10 | 37.0 | 47.12 | 1743.6 | 6,807 | 64.5 | 7,757 | 273.62 | 4.45 | |||||
| APC | 19x12-E | 10 | 37.0 | 55.32 | 2046.7 | 6,545 | 74.4 | 7,852 | 276.97 | 3.84 | |||||
| APC | 20x8-E | 10 | 37.0 | 50.82 | 1880.3 | 6,754 | 51.2 | 8,682 | 306.25 | 4.62 | |||||
| APC | 20x10-E | 10 | 37.0 | 59.91 | 2216.7 | 6,596 | 62.5 | 9,063 | 319.68 | 4.09 | |||||
| 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 | 26.63 | 1182.3 | 8,621 | 65.3 | 4,580 | 161.55 | 3.87 | |||||
| APC | 15x10-E | 12 | 44.4 | 41.43 | 1839.3 | 8,309 | 78.7 | 5,090 | 179.54 | 2.77 | |||||
| APC | 16x8-E | 12 | 44.4 | 46.40 | 2060.3 | 8,232 | 62.4 | 6,167 | 217.53 | 2.99 | |||||
| APC | 16x10-E | 12 | 44.4 | 50.27 | 2232.0 | 8,126 | 77.0 | 6,222 | 219.47 | 2.79 | |||||
| APC | 16x12-E | 12 | 44.4 | 56.24 | 2497.2 | 7,999 | 90.9 | 5,788 | 204.16 | 2.32 | |||||
| APC | 17x8-E | 12 | 44.4 | 48.07 | 2134.2 | 8,192 | 62.1 | 7,046 | 248.54 | 3.30 | |||||
| APC | 17x10-E | 12 | 44.4 | 54.21 | 2406.7 | 7,902 | 74.8 | 7,365 | 259.79 | 3.06 | |||||
| APC | 17x12-E | 12 | 44.4 | 64.39 | 2858.8 | 7,888 | 89.6 | 7,467 | 263.39 | 2.61 | |||||
| APC | 18x8-E | 12 | 44.4 | 47.23 | 2096.9 | 8,209 | 62.2 | 8,785 | 309.88 | 4.19 | |||||
| APC | 18x10-E | 12 | 44.4 | 57.52 | 2553.7 | 8,007 | 75.8 | 8,658 | 305.40 | 3.39 | |||||
| APC | 19x8-E | 12 | 44.4 | 71.48 | 3173.6 | 7,747 | 58.7 | 9,951 | 351.01 | 3.14 | |||||
| APC | 19x10-E | 12 | 44.4 | 66.78 | 2965.0 | 7,842 | 74.3 | 10,196 | 359.65 | 3.44 | |||||
| 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 | |||||||||||||||
| 512 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. | |||||||||||||||