| Cobra C-2217/7 Motor Propeller Data | |||||||||||||||
| Magnets | Motor Wind | Motor Kv | No-Load Current | Motor Resistance | I Max | P Max (4S) | |||||||||
| 14-Pole | 7-Turn Delta | 2500 RPM/Volt | Io = 2.73 Amps @ 10v | Rm = 0.020 Ohms | 50 Amps | 740 W | |||||||||
| Stator | Outside Diameter | Body Length | Total Shaft Length | Shaft Diameter | Motor Weight | ||||||||||
| 12-Slot | 27.8 mm, 1.094 in. | 32.0 mm, 1.259 in. | 47.0 mm, 1.850 in. | 3.17 mm, 0.125 in. | 74.0 gm, 2.61 oz | ||||||||||
| Test Data From | Input | 6.0 V | 8.0 V | 10.0V | 12.0V | Measured Kv value | Measured Rm Value | ||||||||
| Sample Motor | Io Value | 1.956 A | 2.252 A | 2.726 A | 2.862 A | 2563 RPM/Volt @ 10v | 0.0198 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 | 4.75x4.25 | 3 | 11.1 | 24.12 | 267.8 | 25,359 | 102.1 | 566 | 19.96 | 2.11 | |||||
| APC | 4.75x4.75 | 3 | 11.1 | 26.98 | 299.5 | 25,022 | 112.6 | 562 | 19.82 | 1.88 | |||||
| APC | 4.75x5.5-E | 3 | 11.1 | 29.93 | 332.2 | 24,635 | 128.3 | 526 | 18.55 | 1.58 | |||||
| APC | 5x4.3-MR | 3 | 11.1 | 34.19 | 379.5 | 24,170 | 98.4 | 983 | 34.67 | 2.59 | |||||
| APC | 5x4.5-MR | 3 | 11.1 | 34.97 | 388.1 | 24,021 | 102.4 | 967 | 34.11 | 2.49 | |||||
| APC | 5x4.6-MR | 3 | 11.1 | 35.46 | 393.6 | 23,969 | 104.4 | 1031 | 36.37 | 2.62 | |||||
| APC | 5x5-E | 3 | 11.1 | 30.89 | 342.9 | 24,461 | 115.8 | 599 | 21.13 | 1.75 | |||||
| APC | 5.25x4.75-E | 3 | 11.1 | 35.01 | 388.6 | 23,918 | 107.6 | 804 | 28.36 | 2.07 | |||||
| APC | 5.5x4.5-E | 3 | 11.1 | 35.59 | 395.1 | 23,820 | 101.5 | 856 | 30.19 | 2.17 | |||||
| APC | 6x4-E | 3 | 11.1 | 40.33 | 447.6 | 23,344 | 88.4 | 1134 | 40.00 | 2.53 | |||||
| APC | 6x4.3-MR | 3 | 11.1 | 50.15 | 556.7 | 21,685 | 88.3 | 1499 | 52.87 | 2.69 | |||||
| APC | 6x4.5-MR | 3 | 11.1 | 47.96 | 532.3 | 21,991 | 93.7 | 1504 | 53.05 | 2.83 | |||||
| APC | 6x5.5-E | 3 | 11.1 | 48.38 | 537.0 | 21,903 | 114.1 | 1067 | 37.64 | 1.99 | |||||
| HQ | 4x4.5-BN | 3 | 11.1 | 20.89 | 231.9 | 25,822 | 110.0 | 614 | 21.66 | 2.65 | |||||
| HQ | 5x4 | 3 | 11.1 | 20.29 | 225.3 | 25,925 | 98.2 | 768 | 27.09 | 3.41 | |||||
| HQ | 5x4.5 | 3 | 11.1 | 21.61 | 239.8 | 25,714 | 109.6 | 773 | 27.27 | 3.22 | |||||
| HQ | 5x4.5-BN | 3 | 11.1 | 34.18 | 379.4 | 24,167 | 103.0 | 1053 | 37.14 | 2.78 | |||||
| HQ | 6x3 | 3 | 11.1 | 20.68 | 229.6 | 25,900 | 73.6 | 869 | 30.65 | 3.78 | |||||
| HQ | 6x4.5 | 3 | 11.1 | 41.04 | 455.5 | 23,313 | 99.3 | 1410 | 49.74 | 3.10 | |||||
| HQ | 6x4.5-BN | 3 | 11.1 | 52.69 | 584.8 | 21,377 | 91.1 | 1536 | 54.18 | 2.63 | |||||
| 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 | 4x4.5-MR | 4 | 14.8 | 31.21 | 461.9 | 32,783 | 139.7 | 850 | 29.98 | 1.84 | |||||
| APC | 4.1x4.1-E | 4 | 14.8 | 24.16 | 357.5 | 33,728 | 131.0 | 623 | 21.98 | 1.74 | |||||
| APC | 4.5x4.1-E | 4 | 14.8 | 31.25 | 462.5 | 32,705 | 127.0 | 866 | 30.55 | 1.87 | |||||
| APC | 4.75x4.25 | 4 | 14.8 | 37.91 | 561.1 | 31,882 | 128.3 | 897 | 31.64 | 1.60 | |||||
| APC | 4.75x4.75 | 4 | 14.8 | 42.14 | 623.7 | 31,320 | 140.9 | 886 | 31.25 | 1.42 | |||||
| APC | 4.75x5.5-E | 4 | 14.8 | 45.68 | 676.0 | 30,850 | 160.7 | 823 | 29.03 | 1.22 | |||||
| APC | 5x4.3-MR | 4 | 14.8 | 54.18 | 801.9 | 29,818 | 121.4 | 1505 | 53.09 | 1.88 | |||||
| APC | 5x5-E | 4 | 14.8 | 47.66 | 705.4 | 30,538 | 144.6 | 917 | 32.35 | 1.30 | |||||
| APC | 5.25x4.75-E | 4 | 14.8 | 55.34 | 819.1 | 29,571 | 133.0 | 1233 | 43.49 | 1.51 | |||||
| HQ | 4x4.5-BN | 4 | 14.8 | 31.13 | 460.7 | 32,817 | 139.8 | 989 | 34.89 | 2.15 | |||||
| HQ | 5x4 | 4 | 14.8 | 31.11 | 460.5 | 32,850 | 124.4 | 1250 | 44.09 | 2.71 | |||||
| HQ | 5x4.5 | 4 | 14.8 | 33.76 | 499.6 | 32,447 | 138.3 | 1230 | 43.39 | 2.46 | |||||
| HQ | 5x4.5-BN | 4 | 14.8 | 51.38 | 760.5 | 30,212 | 128.7 | 1640 | 57.85 | 2.16 | |||||
| HQ | 6x3 | 4 | 14.8 | 32.99 | 488.3 | 32,624 | 92.7 | 1449 | 51.11 | 2.97 | |||||
| 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. | |||||||||||||||