| Cobra C-5320-22 300Kv Motor Propeller Data | |||||||||||||||
| Magnets | Motor Wind | Motor Kv | No-Load Current | Motor Resistance | I Max | P Max (8S) | |||||||||
| 14-Pole | 22-Turn Delta | 300 RPM/Volt | Io = 1.81 Amps @ 20v | Rm = 0.029 Ohms | 62 Amps | 1835 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 | 1.599 A | 1.811 A | 2.228 A | 2.485 A | 303.6 RPM/Volt @ 20V | 0.0287 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 | 6 | 22.2 | 26.88 | 596.8 | 6,028 | 45.7 | 3,172 | 111.89 | 5.32 | |||||
| APC | 16x10-E | 6 | 22.2 | 30.06 | 667.4 | 5,950 | 56.3 | 3,302 | 116.47 | 4.95 | |||||
| APC | 16x12-E | 6 | 22.2 | 37.07 | 822.9 | 5,785 | 65.7 | 2,958 | 104.34 | 3.59 | |||||
| APC | 17x8-E | 6 | 22.2 | 29.78 | 661.0 | 5,955 | 45.1 | 3,639 | 128.36 | 5.51 | |||||
| APC | 17x10-E | 6 | 22.2 | 36.78 | 816.5 | 5,800 | 54.9 | 3,808 | 134.32 | 4.66 | |||||
| APC | 17x12-E | 6 | 22.2 | 41.58 | 923.1 | 5,726 | 65.1 | 3,743 | 132.03 | 4.05 | |||||
| APC | 18x8-E | 6 | 22.2 | 31.45 | 698.2 | 5,926 | 44.9 | 4,275 | 150.79 | 6.12 | |||||
| APC | 18x10-E | 6 | 22.2 | 37.94 | 842.3 | 5,774 | 54.7 | 4,513 | 159.19 | 5.36 | |||||
| APC | 18x12-E | 6 | 22.2 | 52.56 | 1166.9 | 5,483 | 62.3 | 4,370 | 154.15 | 3.74 | |||||
| APC | 19x8-E | 6 | 22.2 | 43.94 | 975.4 | 5,657 | 42.9 | 5,139 | 181.27 | 5.27 | |||||
| APC | 19x10-E | 6 | 22.2 | 43.48 | 965.2 | 5,659 | 53.6 | 5,201 | 183.46 | 5.39 | |||||
| APC | 19x12-E | 6 | 22.2 | 51.35 | 1139.9 | 5,577 | 63.4 | 5,421 | 191.22 | 4.76 | |||||
| APC | 20x8-E | 6 | 22.2 | 45.22 | 1003.9 | 5,632 | 42.7 | 5,703 | 201.17 | 5.68 | |||||
| APC | 20x10-E | 6 | 22.2 | 53.39 | 1185.3 | 5,474 | 51.8 | 6,076 | 214.32 | 5.13 | |||||
| APC | 20x11-E | 6 | 22.2 | 57.52 | 1276.8 | 5,410 | 56.4 | 5,940 | 209.53 | 4.65 | |||||
| APC | 20x13-E | 6 | 22.2 | 61.44 | 1363.9 | 5,344 | 65.8 | 6,112 | 215.59 | 4.48 | |||||
| APC | 20x15-E | 6 | 22.2 | 75.86 | 1684.0 | 5,208 | 74.0 | 5,558 | 196.05 | 3.30 | |||||
| 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 | 7 | 25.9 | 23.21 | 601.0 | 7,156 | 54.2 | 3,125 | 110.23 | 5.20 | |||||
| APC | 15x10-E | 7 | 25.9 | 34.15 | 884.4 | 6,888 | 65.2 | 3,587 | 126.53 | 4.06 | |||||
| APC | 16x8-E | 7 | 25.9 | 37.00 | 958.3 | 6,813 | 51.6 | 4,180 | 147.44 | 4.36 | |||||
| APC | 16x10-E | 7 | 25.9 | 40.98 | 1061.4 | 6,731 | 63.7 | 4,246 | 149.77 | 4.00 | |||||
| APC | 16x12-E | 7 | 25.9 | 48.60 | 1258.7 | 6,567 | 74.6 | 3,818 | 134.67 | 3.03 | |||||
| APC | 17x8-E | 7 | 25.9 | 40.21 | 1041.4 | 6,755 | 51.2 | 4,719 | 166.46 | 4.53 | |||||
| APC | 17x10-E | 7 | 25.9 | 48.61 | 1259.0 | 6,560 | 62.1 | 4,900 | 172.84 | 3.89 | |||||
| APC | 17x12-E | 7 | 25.9 | 54.69 | 1416.4 | 6,490 | 73.8 | 4,802 | 169.38 | 3.39 | |||||
| APC | 18x8-E | 7 | 25.9 | 40.92 | 1059.7 | 6,724 | 50.9 | 5,519 | 194.67 | 5.21 | |||||
| APC | 18x10-E | 7 | 25.9 | 50.02 | 1295.4 | 6,523 | 61.8 | 5,791 | 204.27 | 4.47 | |||||
| APC | 18x12-E | 7 | 25.9 | 68.91 | 1784.9 | 6,186 | 70.3 | 5,550 | 195.77 | 3.11 | |||||
| APC | 19x8-E | 7 | 25.9 | 58.87 | 1524.6 | 6,350 | 48.1 | 6,619 | 233.48 | 4.34 | |||||
| APC | 19x10-E | 7 | 25.9 | 57.30 | 1484.2 | 6,382 | 60.4 | 6,708 | 236.62 | 4.52 | |||||
| APC | 19x12-E | 7 | 25.9 | 67.76 | 1755.0 | 6,253 | 71.1 | 6,801 | 239.90 | 3.88 | |||||
| APC | 20x8-E | 7 | 25.9 | 60.36 | 1563.2 | 6,333 | 48.0 | 7,389 | 260.64 | 4.73 | |||||
| APC | 20x10-E | 7 | 25.9 | 71.27 | 1845.8 | 6,155 | 58.3 | 7,872 | 277.67 | 4.26 | |||||
| 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 | 27.43 | 811.9 | 8,095 | 46.0 | 3,997 | 140.99 | 4.92 | |||||
| APC | 15x8-E | 8 | 29.6 | 30.18 | 893.4 | 8,010 | 60.7 | 3,972 | 140.11 | 4.45 | |||||
| APC | 15x10-E | 8 | 29.6 | 44.93 | 1329.9 | 7,670 | 72.6 | 4,391 | 154.89 | 3.30 | |||||
| APC | 16x8-E | 8 | 29.6 | 49.15 | 1454.9 | 7,590 | 57.5 | 5,165 | 182.19 | 3.55 | |||||
| APC | 16x10-E | 8 | 29.6 | 54.19 | 1604.1 | 7,442 | 70.5 | 5,207 | 183.67 | 3.25 | |||||
| APC | 16x12-E | 8 | 29.6 | 62.42 | 1847.5 | 7,276 | 82.7 | 4,696 | 165.64 | 2.54 | |||||
| APC | 17x8-E | 8 | 29.6 | 52.76 | 1561.6 | 7,538 | 57.1 | 5,828 | 205.57 | 3.73 | |||||
| APC | 17x10-E | 8 | 29.6 | 62.53 | 1850.9 | 7,343 | 69.5 | 6,066 | 213.97 | 3.28 | |||||
| APC | 18x8-E | 8 | 29.6 | 52.24 | 1546.3 | 7,486 | 56.7 | 6,968 | 245.79 | 4.51 | |||||
| APC | 18x10-E | 8 | 29.6 | 64.73 | 1916.1 | 7,231 | 68.5 | 7,144 | 251.99 | 3.73 | |||||
| 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 | 10 | 37.0 | 44.06 | 1630.0 | 9,684 | 55.0 | 5,785 | 204.06 | 3.55 | |||||
| APC | 15x8-E | 10 | 37.0 | 47.14 | 1744.3 | 9,660 | 73.2 | 5,706 | 201.27 | 3.27 | |||||
| APC | 15x10-E | 10 | 37.0 | 73.46 | 2717.9 | 9,723 | 92.1 | 6,066 | 213.97 | 2.23 | |||||
| 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. | |||||||||||||||