| Cobra CM-2206/20 Motor Propeller Data | |||||||||||||||
| Magnets | Motor Wind | Motor Kv | No-Load Current | Motor Resistance | I Max | P Max (4S) | |||||||||
| 14-Pole | 20-Turn Delta | 2100 RPM/Volt | Io = 0.85 Amps @ 10v | Rm = 0.065 Ohms | 25 Amps | 370 W | |||||||||
| Stator | Outside Diameter | Body Length | Total Shaft Length | Shaft Diameter | Motor Weight | ||||||||||
| 12-Slot | 27.0 mm, 1.063 in. | 16.5 mm, 1.102 in. | 35.3 mm, 1.390 in. | 3.00 mm, 0.118 in. | 36.5 gm, 1.29 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 | 0.66 A | 0.76 A | 0.85 A | 0.95 A | 2091 RPM/Volt @ 10v | 0.065 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 | 5.25x4.75-E | 3 | 11.1 | 14.43 | 160.2 | 17,849 | 80.3 | 466 | 16.44 | 2.91 | |||||
| APC | 5.5x4.5-E | 3 | 11.1 | 14.94 | 165.8 | 17,747 | 75.6 | 481 | 16.97 | 2.90 | |||||
| APC | 6x4-E | 3 | 11.1 | 16.38 | 181.8 | 17,285 | 65.5 | 620 | 21.87 | 3.41 | |||||
| APC | 7x4-SF | 3 | 11.1 | 25.33 | 281.2 | 14,747 | 55.9 | 917 | 32.35 | 3.26 | |||||
| FC | 5x4.5 | 3 | 11.1 | 8.94 | 99.2 | 19,120 | 85.1 | 429 | 15.13 | 4.32 | |||||
| FC | 5x4.5x3 | 3 | 11.1 | 13.43 | 149.1 | 18,125 | 80.7 | 555 | 19.58 | 3.72 | |||||
| FC | 6x4.5 | 3 | 11.1 | 16.96 | 188.3 | 17,189 | 76.5 | 749 | 26.42 | 3.98 | |||||
| GemFan | 5x3 | 3 | 11.1 | 6.74 | 74.8 | 19,714 | 56.0 | 381 | 13.44 | 5.09 | |||||
| HQ | 4x4.5-BN | 3 | 11.1 | 8.69 | 96.5 | 19,260 | 85.7 | 353 | 12.45 | 3.66 | |||||
| HQ | 5x3 | 3 | 11.1 | 5.09 | 56.5 | 20,450 | 58.1 | 291 | 10.26 | 5.15 | |||||
| HQ | 5x4 | 3 | 11.1 | 8.73 | 96.9 | 19,175 | 72.6 | 445 | 15.70 | 4.59 | |||||
| HQ | 5x4.5-BN | 3 | 11.1 | 13.92 | 154.5 | 18,180 | 80.9 | 572 | 20.18 | 3.70 | |||||
| HQ | 6x3 | 3 | 11.1 | 8.78 | 97.5 | 19,261 | 54.7 | 495 | 17.46 | 5.08 | |||||
| HQ | 6x4.5 | 3 | 11.1 | 16.98 | 188.5 | 17,233 | 76.7 | 762 | 26.88 | 4.04 | |||||
| HQ | 6x4.5x3 | 3 | 11.1 | 21.27 | 236.1 | 15,917 | 70.8 | 844 | 29.77 | 3.57 | |||||
| HQ | 7x4-SF | 3 | 11.1 | 25.30 | 280.8 | 14,772 | 56.0 | 942 | 33.23 | 3.35 | |||||
| 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 | 5.25x4.75-E | 4 | 14.8 | 21.87 | 323.7 | 21,797 | 98.0 | 692 | 24.41 | 2.14 | |||||
| APC | 5.5x4.5-E | 4 | 14.8 | 22.55 | 333.7 | 21,573 | 91.9 | 716 | 25.26 | 2.15 | |||||
| APC | 6x4-E | 4 | 14.8 | 24.48 | 362.3 | 20,848 | 79.0 | 912 | 32.17 | 2.52 | |||||
| FC | 5x4.5 | 4 | 14.8 | 13.65 | 202.0 | 23,732 | 101.1 | 685 | 24.16 | 3.39 | |||||
| FC | 5x4.5x3 | 4 | 14.8 | 20.00 | 296.0 | 22,341 | 95.2 | 845 | 29.81 | 2.85 | |||||
| FC | 6x4.5 | 4 | 14.8 | 24.86 | 367.9 | 20,696 | 88.2 | 1114 | 39.29 | 3.03 | |||||
| GemFan | 5x3 | 4 | 14.8 | 9.61 | 142.2 | 24,158 | 68.6 | 587 | 20.71 | 4.13 | |||||
| HQ | 4x4.5-BN | 4 | 14.8 | 12.61 | 186.6 | 23,927 | 102.0 | 549 | 19.37 | 2.94 | |||||
| HQ | 5x3 | 4 | 14.8 | 7.82 | 115.7 | 25,301 | 71.9 | 465 | 16.40 | 4.02 | |||||
| HQ | 5x4 | 4 | 14.8 | 12.98 | 192.1 | 23,857 | 90.4 | 695 | 24.52 | 3.62 | |||||
| HQ | 5x4.5-BN | 4 | 14.8 | 20.40 | 301.9 | 22,356 | 95.3 | 857 | 30.23 | 2.84 | |||||
| HQ | 6x3 | 4 | 14.8 | 13.99 | 207.1 | 23,658 | 67.2 | 818 | 28.85 | 3.95 | |||||
| HQ | 6x4.5 | 4 | 14.8 | 24.18 | 357.9 | 21,021 | 89.6 | 1100 | 38.80 | 3.07 | |||||
| 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. | |||||||||||||||