| BadAss BA-2315-1800 Performance Test Data | |||||||||||||||
| Magnets | Motor Wind | Motor Kv | No-Load Current | Motor Resistance | I Max | P Max (5S) | |||||||||
| 14-Pole | 10-Turn Delta | 1800 RPM/Volt | Io = 1.98 Amps @ 10v | Rm = 0.027 Ohms | 44 Amps | 810 W | |||||||||
| Stator | Outside Diameter | Body Length | Total Shaft Length | Shaft Diameter | Motor Weight | ||||||||||
| 12-Slot | 29.1 mm, 1.146 in. | 32.6 mm, 1.283 in. | 51.0 mm, 2.008 in. | 4.00 mm, 0.157 in. | 75.2 gm, 2.65 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 | 1.714 A | 1.982 A | 2.231 A | 2.538 A | 1825 RPM/Volt @ 10v | 0.0267 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 | 7x6-E | 2 | 7.4 | 20.17 | 149.3 | 11,736 | 66.7 | 660 | 23.28 | 4.42 | |||||
| APC | 7x6-F | 2 | 7.4 | 16.91 | 125.1 | 11,924 | 67.8 | 413 | 14.57 | 3.30 | |||||
| APC | 7x7-E | 2 | 7.4 | 24.30 | 179.8 | 11,344 | 75.2 | 662 | 23.35 | 3.68 | |||||
| APC | 8x4-E | 2 | 7.4 | 22.41 | 165.8 | 11,526 | 43.7 | 825 | 29.10 | 4.98 | |||||
| APC | 8x4-F | 2 | 7.4 | 16.51 | 122.1 | 11,815 | 44.8 | 571 | 20.15 | 4.68 | |||||
| APC | 8x6-E | 2 | 7.4 | 31.21 | 230.9 | 10,638 | 60.4 | 917 | 32.34 | 3.97 | |||||
| APC | 8x8-E | 2 | 7.4 | 40.29 | 298.2 | 9,691 | 73.4 | 792 | 27.93 | 2.66 | |||||
| APC | 9x4.5-E | 2 | 7.4 | 30.56 | 226.2 | 10,680 | 45.5 | 1100 | 38.80 | 4.86 | |||||
| APC | 9x5-F | 2 | 7.4 | 26.28 | 194.5 | 10,901 | 51.6 | 906 | 31.97 | 4.66 | |||||
| APC | 9x6-E | 2 | 7.4 | 35.19 | 260.4 | 10,244 | 58.2 | 1096 | 38.66 | 4.21 | |||||
| APC | 9x7.5-E | 2 | 7.4 | 45.59 | 337.3 | 9,036 | 64.2 | 1040 | 36.68 | 3.08 | |||||
| APC | 9x9-E | 2 | 7.4 | 53.41 | 395.2 | 8,713 | 74.3 | 987 | 34.80 | 2.50 | |||||
| APC | 10x5-E | 2 | 7.4 | 39.56 | 292.8 | 9,736 | 46.1 | 1320 | 46.56 | 4.51 | |||||
| APC | 10x6-E | 2 | 7.4 | 42.48 | 314.4 | 9,381 | 53.3 | 1313 | 46.31 | 4.18 | |||||
| APC | 10x6-F | 2 | 7.4 | 35.17 | 260.3 | 9,849 | 56.0 | 1134 | 39.99 | 4.36 | |||||
| APC | 10x7-E | 2 | 7.4 | 48.49 | 358.8 | 9,053 | 60.0 | 1340 | 47.28 | 3.74 | |||||
| MAS | 7x4x3 | 2 | 7.4 | 16.93 | 125.3 | 12,054 | 45.7 | 578 | 20.37 | 4.61 | |||||
| MAS | 8x6x3 | 2 | 7.4 | 31.38 | 232.2 | 10,602 | 60.2 | 987 | 34.80 | 4.25 | |||||
| MAS | 9x7x3 | 2 | 7.4 | 45.11 | 333.8 | 9,373 | 62.1 | 1301 | 45.89 | 3.90 | |||||
| MAS | 10x5x3 | 2 | 7.4 | 40.97 | 303.2 | 9,536 | 45.2 | 1338 | 47.19 | 4.41 | |||||
| 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 | 6x4-E | 3 | 11.1 | 18.26 | 202.7 | 18,256 | 69.2 | 667 | 23.52 | 3.29 | |||||
| APC | 6x4.3-E | 3 | 11.1 | 24.91 | 276.5 | 17,512 | 71.3 | 959 | 33.83 | 3.47 | |||||
| APC | 6x4.5-E | 3 | 11.1 | 23.98 | 266.1 | 17,749 | 75.6 | 958 | 33.79 | 3.60 | |||||
| APC | 6x5.5-E | 3 | 11.1 | 24.01 | 266.5 | 17,735 | 92.4 | 674 | 23.77 | 2.53 | |||||
| APC | 6x6-E | 3 | 11.1 | 25.84 | 286.8 | 17,661 | 100.3 | 756 | 26.67 | 2.64 | |||||
| APC | 7x4-E | 3 | 11.1 | 31.65 | 351.3 | 16,985 | 64.3 | 1252 | 44.17 | 3.57 | |||||
| APC | 7x4-F | 3 | 11.1 | 23.19 | 257.4 | 17,672 | 66.9 | 753 | 26.56 | 2.93 | |||||
| APC | 7x5-E | 3 | 11.1 | 38.35 | 425.6 | 16,194 | 76.7 | 1198 | 42.27 | 2.82 | |||||
| APC | 7x6-E | 3 | 11.1 | 39.23 | 435.5 | 16,098 | 91.5 | 1288 | 45.44 | 2.96 | |||||
| APC | 7x6-F | 3 | 11.1 | 31.93 | 354.5 | 16,635 | 94.5 | 846 | 29.82 | 2.39 | |||||
| APC | 7x7-E | 3 | 11.1 | 46.07 | 511.3 | 15,257 | 101.1 | 1203 | 42.43 | 2.35 | |||||
| APC | 8x4-E | 3 | 11.1 | 43.79 | 486.0 | 15,538 | 58.9 | 1569 | 55.33 | 3.23 | |||||
| APC | 8x6-E | 3 | 11.1 | 61.47 | 682.3 | 13,905 | 79.0 | 1604 | 56.57 | 2.35 | |||||
| APC | 9x4.5-E | 3 | 11.1 | 58.84 | 653.1 | 13,882 | 59.2 | 2120 | 74.78 | 3.25 | |||||
| MAS | 6x4x3 | 3 | 11.1 | 23.85 | 264.7 | 18,395 | 69.7 | 769 | 27.12 | 2.90 | |||||
| MAS | 7x4x3 | 3 | 11.1 | 32.40 | 359.7 | 16,903 | 64.0 | 1205 | 42.49 | 3.35 | |||||
| MAS | 8x6x3 | 3 | 11.1 | 56.89 | 631.5 | 14,411 | 81.9 | 1867 | 65.84 | 2.96 | |||||
| 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 | 4.75x4.75-E | 4 | 14.8 | 20.32 | 300.7 | 25,029 | 112.6 | 549 | 19.35 | 1.82 | |||||
| APC | 4.75x5.5-E | 4 | 14.8 | 22.81 | 337.6 | 24,684 | 128.6 | 517 | 18.24 | 1.53 | |||||
| APC | 5x4.3-E | 4 | 14.8 | 26.39 | 390.5 | 24,160 | 98.4 | 972 | 34.29 | 2.49 | |||||
| APC | 5x4.5-E | 4 | 14.8 | 27.90 | 412.9 | 24,056 | 102.5 | 971 | 34.26 | 2.35 | |||||
| APC | 5x4.6-E | 4 | 14.8 | 27.65 | 409.2 | 24,068 | 104.8 | 1038 | 36.60 | 2.54 | |||||
| APC | 5x5-E | 4 | 14.8 | 23.27 | 344.5 | 24,584 | 116.4 | 575 | 20.28 | 1.67 | |||||
| APC | 5.25x4.75-E | 4 | 14.8 | 27.45 | 406.2 | 24,079 | 108.3 | 811 | 28.59 | 2.00 | |||||
| APC | 5.25x6.25-E | 4 | 14.8 | 34.54 | 511.3 | 23,224 | 137.5 | 761 | 26.83 | 1.49 | |||||
| APC | 5.5x4.5-E | 4 | 14.8 | 28.15 | 416.6 | 24,028 | 102.4 | 861 | 30.35 | 2.07 | |||||
| APC | 6x4-E | 4 | 14.8 | 31.87 | 471.7 | 23,571 | 89.3 | 1142 | 40.28 | 2.42 | |||||
| APC | 6x4.3-E | 4 | 14.8 | 40.63 | 601.4 | 22,176 | 90.3 | 1554 | 54.83 | 2.58 | |||||
| APC | 6x4.5-E | 4 | 14.8 | 38.40 | 568.2 | 22,560 | 96.1 | 1565 | 55.21 | 2.75 | |||||
| APC | 6x5.5-E | 4 | 14.8 | 39.20 | 580.2 | 22,489 | 117.1 | 1086 | 38.29 | 1.87 | |||||
| APC | 6x6-E | 4 | 14.8 | 42.32 | 626.3 | 22,033 | 125.2 | 1194 | 42.13 | 1.91 | |||||
| APC | 7x4-E | 4 | 14.8 | 53.68 | 794.5 | 20,892 | 79.1 | 1952 | 68.85 | 2.46 | |||||
| 5-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 | 4.5x4.1-E | 5 | 18.5 | 21.76 | 402.6 | 31,204 | 121.2 | 778 | 27.43 | 1.93 | |||||
| APC | 4.7x4.25-E | 5 | 18.5 | 26.77 | 495.2 | 30,517 | 122.8 | 810 | 28.57 | 1.64 | |||||
| APC | 4.75x4.75-E | 5 | 18.5 | 30.10 | 556.9 | 30,164 | 135.7 | 804 | 28.35 | 1.44 | |||||
| APC | 4.75x5.5-E | 5 | 18.5 | 32.68 | 604.6 | 29,779 | 155.1 | 752 | 26.53 | 1.24 | |||||
| APC | 5x4.3-E | 5 | 18.5 | 39.13 | 723.9 | 28,890 | 117.6 | 1404 | 49.51 | 1.94 | |||||
| APC | 5x4.5-E | 5 | 18.5 | 42.43 | 785.0 | 28,483 | 121.4 | 1390 | 49.02 | 1.77 | |||||
| APC | 5x4.6-E | 5 | 18.5 | 40.68 | 752.5 | 28,636 | 124.7 | 1495 | 52.72 | 1.99 | |||||
| APC | 5x5-E | 5 | 18.5 | 34.36 | 635.7 | 29,579 | 140.1 | 850 | 29.99 | 1.34 | |||||
| APC | 5.25x4.75-E | 5 | 18.5 | 40.42 | 747.8 | 28,769 | 129.4 | 1152 | 40.64 | 1.54 | |||||
| APC | 5.25x6.25-E | 5 | 18.5 | 49.26 | 911.2 | 27,788 | 164.5 | 1091 | 38.50 | 1.20 | |||||
| APC | 5.5x4.5-E | 5 | 18.5 | 40.98 | 758.1 | 28,518 | 121.5 | 1238 | 43.68 | 1.63 | |||||
| APC | 6x4-E | 5 | 18.5 | 47.58 | 880.1 | 27,920 | 105.8 | 1611 | 56.81 | 1.83 | |||||
| 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. | |||||||||||||||