| BadAss BA-2310-2350 Performance Test Data | |||||||||||||||
| Magnets | Motor Wind | Motor Kv | No-Load Current | Motor Resistance | I Max | P Max (4S) | |||||||||
| 14-Pole | 12-Turn Delta | 2350 RPM/Volt | Io = 2.34 Amps @ 10v | Rm = 0.029 Ohms | 42 Amps | 620 W | |||||||||
| Stator | Outside Diameter | Body Length | Total Shaft Length | Shaft Diameter | Motor Weight | ||||||||||
| 12-Slot | 29.1 mm, 1.146 in. | 27.6 mm, 1.087 in. | 46.0 mm, 1.811 in. | 4.00 mm, 0.157 in. | 58.2 gm, 2.05 oz | ||||||||||
| Test Data From | Input | 8.0 V | 10.0 V | 12.0V | 14.0V | Measured Kv value | Measured Rm Value | ||||||||
| Sample Motor | Io Value | 1.873 A | 2.337 A | 2.582 A | 2.756 A | 2368 RPM/Volt @ 10v | 0.0293 Ohms | ||||||||
| 2-cell Li-Po Test Data | |||||||||||||||
| 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 | 6x4-E | 2 | 7.4 | 15.83 | 117.1 | 15,313 | 58.0 | 470 | 16.57 | 4.01 | |||||
| APC | 6x4.3-E | 2 | 7.4 | 21.61 | 159.9 | 14,580 | 59.4 | 649 | 22.90 | 4.06 | |||||
| APC | 6x4.5-E | 2 | 7.4 | 20.94 | 155.0 | 14,648 | 62.4 | 657 | 23.19 | 4.24 | |||||
| APC | 6x5.5-E | 2 | 7.4 | 19.58 | 144.9 | 14,844 | 77.3 | 505 | 17.81 | 3.49 | |||||
| APC | 6x6-E | 2 | 7.4 | 21.56 | 159.5 | 14,564 | 82.8 | 523 | 18.43 | 3.28 | |||||
| APC | 7x4-E | 2 | 7.4 | 25.72 | 190.3 | 13,977 | 52.9 | 811 | 28.60 | 4.26 | |||||
| APC | 7x5-E | 2 | 7.4 | 30.95 | 229.0 | 13,218 | 62.6 | 776 | 27.38 | 3.39 | |||||
| APC | 7x6-E | 2 | 7.4 | 32.06 | 237.2 | 13,068 | 74.3 | 836 | 29.50 | 3.53 | |||||
| APC | 7x7-E | 2 | 7.4 | 36.72 | 271.7 | 12,370 | 82.0 | 779 | 27.47 | 2.87 | |||||
| APC | 8x4-E | 2 | 7.4 | 34.56 | 255.7 | 12,666 | 48.0 | 1014 | 35.78 | 3.97 | |||||
| APC | 8x6-E | 2 | 7.4 | 46.19 | 341.8 | 11,363 | 64.6 | 1046 | 36.91 | 3.06 | |||||
| 3-cell Li-Po Test Data | |||||||||||||||
| 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 | 4.7x4.25-E | 3 | 11.1 | 18.97 | 210.5 | 23,174 | 93.3 | 457 | 16.13 | 2.17 | |||||
| APC | 4.75x4.75-E | 3 | 11.1 | 21.61 | 239.9 | 22,955 | 103.3 | 462 | 16.29 | 1.92 | |||||
| APC | 4.75x5.5-E | 3 | 11.1 | 23.71 | 263.2 | 22,454 | 116.9 | 425 | 15.01 | 1.62 | |||||
| APC | 5x4.3-E | 3 | 11.1 | 25.81 | 286.5 | 21,677 | 88.3 | 782 | 27.57 | 2.73 | |||||
| APC | 5x4.5-E | 3 | 11.1 | 26.79 | 297.4 | 21,474 | 91.5 | 775 | 27.33 | 2.61 | |||||
| APC | 5x4.6-E | 3 | 11.1 | 26.82 | 297.7 | 21,509 | 93.7 | 821 | 28.96 | 2.76 | |||||
| APC | 5x5-E | 3 | 11.1 | 23.55 | 261.4 | 22,091 | 104.6 | 470 | 16.58 | 1.80 | |||||
| APC | 5.25x4.75-E | 3 | 11.1 | 26.71 | 296.5 | 21,530 | 96.8 | 649 | 22.89 | 2.19 | |||||
| APC | 5.25x6.25-E | 3 | 11.1 | 34.03 | 377.8 | 20,555 | 121.7 | 597 | 21.07 | 1.58 | |||||
| APC | 5.5x4.5-E | 3 | 11.1 | 28.24 | 313.4 | 21,804 | 92.9 | 701 | 24.74 | 2.24 | |||||
| APC | 6x4-E | 3 | 11.1 | 31.59 | 350.7 | 21,232 | 80.4 | 923 | 32.55 | 2.63 | |||||
| APC | 6x4.3-E | 3 | 11.1 | 39.91 | 443.0 | 19,840 | 80.8 | 1234 | 43.54 | 2.79 | |||||
| APC | 6x4.5-E | 3 | 11.1 | 38.22 | 424.3 | 20,143 | 85.8 | 1237 | 43.64 | 2.92 | |||||
| APC | 6x5.5-E | 3 | 11.1 | 37.07 | 411.5 | 20,331 | 105.9 | 967 | 34.11 | 2.35 | |||||
| APC | 6x6-E | 3 | 11.1 | 40.99 | 455.0 | 19,701 | 111.9 | 954 | 33.66 | 2.10 | |||||
| APC | 7x4-E | 3 | 11.1 | 50.15 | 556.7 | 18,688 | 70.8 | 1534 | 54.12 | 2.76 | |||||
| 4-cell Li-Po Test Data | |||||||||||||||
| 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 | 4.1x4.1-E | 4 | 14.8 | 19.88 | 294.3 | 31,372 | 121.8 | 535 | 18.85 | 1.82 | |||||
| APC | 4.5x4.1-E | 4 | 14.8 | 25.74 | 381.0 | 30,433 | 118.2 | 739 | 26.06 | 1.94 | |||||
| APC | 4.7x4.25-E | 4 | 14.8 | 31.44 | 465.3 | 29,635 | 119.3 | 758 | 26.73 | 1.63 | |||||
| APC | 4.75x4.75-E | 4 | 14.8 | 35.23 | 521.4 | 28,982 | 130.4 | 745 | 26.29 | 1.43 | |||||
| APC | 4.75x5.5-E | 4 | 14.8 | 38.01 | 562.5 | 28,484 | 148.4 | 688 | 24.28 | 1.22 | |||||
| APC | 5x4.3-E | 4 | 14.8 | 44.75 | 662.3 | 27,600 | 112.4 | 1277 | 45.04 | 1.93 | |||||
| APC | 5x4.5-E | 4 | 14.8 | 47.67 | 705.4 | 27,150 | 115.7 | 1259 | 44.40 | 1.78 | |||||
| APC | 5x4.6-E | 4 | 14.8 | 46.13 | 682.7 | 27,321 | 119.0 | 1355 | 47.80 | 1.99 | |||||
| APC | 5x5-E | 4 | 14.8 | 39.24 | 580.8 | 28,253 | 133.8 | 759 | 26.78 | 1.31 | |||||
| APC | 5.25x4.75-E | 4 | 14.8 | 46.24 | 684.3 | 26,804 | 120.6 | 1034 | 36.46 | 1.51 | |||||
| APC | 5.5x4.5-E | 4 | 14.8 | 46.41 | 686.9 | 27,400 | 116.8 | 1114 | 39.28 | 1.62 | |||||
| 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. | |||||||||||||||