| Cobra CM-1806-26 Motor Propeller Data | |||||||||||||||
| Magnets | Motor Wind | Motor Kv | No-Load Current | Motor Resistance | I Max | P Max (4S) | |||||||||
| 14-Pole | 26-Turn Delta | 2800 RPM/Volt | Io = 0.653 Amps @ 10v | Rm = 0.078 Ohms | 15 Amps | 220 W | |||||||||
| Stator | Outside Diameter | Body Length | Total Shaft Length | Shaft Diameter | Motor Weight | ||||||||||
| 12-Slot | 23.0 mm, 0.906 in. | 15.1 mm, 0.594 in. | 33.1 mm, 1.303 in. | 2.00 mm, 0.079 in. | 21.0 gm, 0.74 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 | 0.505 A | 0.559 A | 0.653 A | 0.687 A | 2818 RPM/Volt @ 10v | 0.078 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 | |||||
| HQ | 4x4-BN | 3 | 11.1 | 11.75 | 130.4 | 23,260 | 88.1 | 420.5 | 14.83 | 3.22 | |||||
| HQ | 4x4x3-BN | 3 | 11.1 | 14.45 | 160.4 | 22,511 | 85.3 | 478.1 | 16.86 | 2.98 | |||||
| HQ | 4x4.5 | 3 | 11.1 | 8.28 | 91.9 | 25,727 | 109.6 | 318.7 | 11.24 | 3.47 | |||||
| HQ | 4x4.5-BN | 3 | 11.1 | 15.54 | 172.5 | 21,998 | 93.7 | 471.0 | 16.61 | 2.73 | |||||
| HQ | 5x3 | 3 | 11.1 | 10.80 | 119.9 | 24,598 | 69.9 | 503.5 | 17.76 | 4.20 | |||||
| HQ | 5x4 | 3 | 11.1 | 14.87 | 165.1 | 22,461 | 85.1 | 591.5 | 20.86 | 3.58 | |||||
| HQ | 5x4.5 | 3 | 11.1 | 15.61 | 173.3 | 22,033 | 93.9 | 596.7 | 21.05 | 3.44 | |||||
| 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 | |||||
| HQ | 3x3 | 4 | 14.8 | 8.05 | 119.1 | 35,238 | 100.1 | 321.6 | 11.34 | 2.70 | |||||
| HQ | 4x4 | 4 | 14.8 | 18.11 | 268.0 | 29,440 | 111.5 | 624.5 | 22.03 | 2.33 | |||||
| HQ | 4x4.5 | 4 | 14.8 | 12.97 | 192.0 | 32,319 | 137.7 | 493.9 | 17.42 | 2.57 | |||||
| HQ | 5x3 | 4 | 14.8 | 15.61 | 231.0 | 29,665 | 84.3 | 738.4 | 26.05 | 3.20 | |||||
| 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. | |||||||||||||||