| Cobra C-5340-20 160Kv Motor Propeller Data | |||||||||||||||
| Magnets | Motor Wind | Motor Kv | No-Load Current | Motor Resistance | I Max | P Max (12S) | |||||||||
| 14-Pole | 20-Turn Delta | 160 RPM/Volt | Io = 1.63 Amps @ 20v | Rm = 0.035 Ohms | 54 Amps | 2400 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. | 818 grams, 28.85 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 | 1.463 A | 1.630 A | 1.760 A | 1.942 A | 165.8 RPM/Volt @ 20V | 0.0355 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 | 17x12-E | 10 | 37.0 | 24.66 | 912.5 | 5,708 | 64.9 | 3,813 | 134.50 | 4.18 | |||||
| APC | 18x10-E | 10 | 37.0 | 22.12 | 818.4 | 5,753 | 54.5 | 4,420 | 155.91 | 5.40 | |||||
| APC | 18x12-E | 10 | 37.0 | 31.94 | 1181.6 | 5,600 | 63.6 | 4,570 | 161.20 | 3.87 | |||||
| APC | 19x8-E | 10 | 37.0 | 26.16 | 967.8 | 5,684 | 43.1 | 5,174 | 182.51 | 5.35 | |||||
| APC | 19x10-E | 10 | 37.0 | 26.00 | 961.8 | 5,700 | 54.0 | 5,303 | 187.06 | 5.51 | |||||
| APC | 19x12-E | 10 | 37.0 | 31.07 | 1149.7 | 5,614 | 63.8 | 5,684 | 200.50 | 4.94 | |||||
| APC | 20x8-E | 10 | 37.0 | 26.98 | 998.2 | 5,669 | 42.9 | 5,779 | 203.85 | 5.79 | |||||
| APC | 20x10-E | 10 | 37.0 | 32.48 | 1201.6 | 5,596 | 53.0 | 6,334 | 223.42 | 5.27 | |||||
| APC | 20x11-E | 10 | 37.0 | 35.56 | 1315.6 | 5,550 | 57.8 | 6,376 | 224.90 | 4.85 | |||||
| APC | 20x13-E | 10 | 37.0 | 37.89 | 1401.9 | 5,511 | 67.8 | 6,605 | 232.98 | 4.71 | |||||
| APC | 20x15-E | 10 | 37.0 | 47.14 | 1744.2 | 5,442 | 77.3 | 6,225 | 219.58 | 3.57 | |||||
| APC | 21x12W-E | 10 | 37.0 | 44.92 | 1662.0 | 5,412 | 61.5 | 7,972 | 281.20 | 4.80 | |||||
| APC | 21x14-E | 10 | 37.0 | 42.36 | 1567.5 | 5,450 | 72.3 | 7,673 | 270.65 | 4.90 | |||||
| APC | 22x10-E | 10 | 37.0 | 42.66 | 1578.3 | 5,441 | 51.5 | 8,064 | 284.45 | 5.11 | |||||
| APC | 22x12-E | 10 | 37.0 | 52.90 | 1957.2 | 5,300 | 60.2 | 8,642 | 304.83 | 4.42 | |||||
| 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 | 12 | 44.4 | 22.58 | 1002.6 | 6,893 | 52.2 | 4,332 | 152.81 | 4.32 | |||||
| APC | 16x10-E | 12 | 44.4 | 25.37 | 1126.3 | 6,852 | 64.9 | 4,459 | 157.28 | 3.96 | |||||
| APC | 16x12-E | 12 | 44.4 | 30.87 | 1370.8 | 6,781 | 77.1 | 4,157 | 146.63 | 3.03 | |||||
| APC | 17x8-E | 12 | 44.4 | 24.77 | 1099.8 | 6,861 | 52.0 | 4,946 | 174.46 | 4.50 | |||||
| APC | 17x10-E | 12 | 44.4 | 30.51 | 1354.7 | 6,759 | 64.0 | 5,323 | 187.76 | 3.93 | |||||
| APC | 17x12-E | 12 | 44.4 | 34.82 | 1545.8 | 6,700 | 76.1 | 5,261 | 185.57 | 3.40 | |||||
| APC | 18x8-E | 12 | 44.4 | 25.45 | 1130.2 | 6,855 | 51.9 | 5,871 | 207.09 | 5.19 | |||||
| APC | 18x10-E | 12 | 44.4 | 31.29 | 1389.3 | 6,754 | 64.0 | 6,193 | 218.45 | 4.46 | |||||
| APC | 18x12-E | 12 | 44.4 | 44.88 | 1992.5 | 6,556 | 74.5 | 6,331 | 223.32 | 3.18 | |||||
| APC | 19x8-E | 12 | 44.4 | 38.37 | 1703.6 | 6,677 | 50.6 | 7,264 | 256.23 | 4.26 | |||||
| APC | 19x10-E | 12 | 44.4 | 36.81 | 1634.3 | 6,648 | 63.0 | 7,324 | 258.34 | 4.48 | |||||
| APC | 19x12-E | 12 | 44.4 | 44.46 | 1974.0 | 6,554 | 74.5 | 7,789 | 274.75 | 3.95 | |||||
| APC | 20x8-E | 12 | 44.4 | 38.85 | 1725.0 | 6,637 | 50.3 | 8,096 | 285.58 | 4.69 | |||||
| APC | 20x10-E | 12 | 44.4 | 46.97 | 2085.5 | 6,522 | 61.8 | 8,709 | 307.20 | 4.18 | |||||
| APC | 20x11-E | 12 | 44.4 | 50.23 | 2230.0 | 6,513 | 67.8 | 8,701 | 306.92 | 3.90 | |||||
| APC | 20x13-E | 12 | 44.4 | 53.85 | 2390.8 | 6,498 | 80.0 | 8,955 | 315.88 | 3.75 | |||||
| APC | 20x15-E | 12 | 44.4 | 62.66 | 2782.1 | 6,347 | 90.2 | 8,411 | 296.69 | 3.02 | |||||
| APC | 21x12W-E | 12 | 44.4 | 63.03 | 2798.5 | 6,271 | 71.3 | 10,671 | 376.40 | 3.81 | |||||
| APC | 22x10-E | 12 | 44.4 | 61.24 | 2719.1 | 6,287 | 59.5 | 10,802 | 381.03 | 3.97 | |||||
| XOAR | 22x10-W | 12 | 44.4 | 59.46 | 2640.0 | 6,453 | 61.1 | 10,888 | 384.06 | 4.12 | |||||
| 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. | |||||||||||||||