| BadAss BA-2305-1960 Performance Test Data | |||||||||||||||
| Magnets | Motor Wind | Motor Kv | No-Load Current | Motor Resistance | I Max | P Max (4S) | |||||||||
| 14-Pole | 28-Turn Delta | 1960 RPM/Volt | Io = 0.83 Amps @ 10v | Rm = 0.084 Ohms | 20 Amps | 300 W | |||||||||
| Stator | Outside Diameter | Body Length | Total Shaft Length | Shaft Diameter | Motor Weight | ||||||||||
| 12-Slot | 29.1 mm, 1.146 in. | 22.6 mm, 0.890 in. | 41.0 mm, 1.614 in. | 4.00 mm, 0.157 in. | 40.6 gm, 1.43 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 | 0.727 A | 0.831 A | 1.098 A | 1.252 A | 1958 RPM/Volt @ 10v | 0.0839 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 | 5x4.6-E | 2 | 7.4 | 7.63 | 56.4 | 12,560 | 54.7 | 274 | 9.66 | 4.85 | |||||
| APC | 6x4-E | 2 | 7.4 | 8.38 | 62.0 | 12,350 | 46.8 | 301 | 10.60 | 4.85 | |||||
| APC | 6x4.3-E | 2 | 7.4 | 11.24 | 83.2 | 11,595 | 47.2 | 418 | 14.74 | 5.02 | |||||
| APC | 6x4.5-E | 2 | 7.4 | 10.92 | 80.8 | 11,684 | 49.8 | 417 | 14.70 | 5.16 | |||||
| APC | 6x5.5-E | 2 | 7.4 | 10.97 | 81.2 | 11,659 | 60.7 | 295 | 10.42 | 3.64 | |||||
| APC | 6x6-E | 2 | 7.4 | 11.11 | 82.2 | 11,630 | 66.1 | 340 | 12.00 | 4.14 | |||||
| APC | 7x4-E | 2 | 7.4 | 12.78 | 94.6 | 11,155 | 42.3 | 502 | 17.70 | 5.30 | |||||
| APC | 7x4-SF | 2 | 7.4 | 13.15 | 97.3 | 11,044 | 41.8 | 487 | 17.17 | 5.00 | |||||
| APC | 7x5-E | 2 | 7.4 | 15.20 | 112.5 | 10,416 | 49.3 | 476 | 16.78 | 4.23 | |||||
| APC | 7x5-SF | 2 | 7.4 | 15.02 | 111.2 | 10,490 | 49.7 | 495 | 17.45 | 4.45 | |||||
| APC | 7x6-E | 2 | 7.4 | 15.73 | 116.4 | 10,236 | 58.2 | 497 | 17.54 | 4.27 | |||||
| APC | 7x6-SF | 2 | 7.4 | 17.22 | 127.4 | 9,777 | 55.6 | 458 | 16.15 | 3.59 | |||||
| APC | 7x7-E | 2 | 7.4 | 17.91 | 132.5 | 9,521 | 63.1 | 475 | 16.75 | 3.58 | |||||
| APC | 8x3.8-SF | 2 | 7.4 | 18.34 | 135.7 | 9,364 | 33.7 | 624 | 22.01 | 4.60 | |||||
| APC | 8x4-E | 2 | 7.4 | 16.79 | 124.3 | 9,899 | 37.5 | 602 | 21.23 | 4.84 | |||||
| APC | 8x4.7-SF | 2 | 7.4 | 19.16 | 141.8 | 8,989 | 40.0 | 637 | 22.47 | 4.49 | |||||
| APC | 8x6-E | 2 | 7.4 | 21.37 | 158.1 | 8,716 | 49.5 | 563 | 19.86 | 3.56 | |||||
| 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 | 9.77 | 108.4 | 18,859 | 75.9 | 310 | 10.95 | 2.86 | |||||
| APC | 4.75x4.75-E | 3 | 11.1 | 10.83 | 120.2 | 18,554 | 83.5 | 308 | 10.85 | 2.56 | |||||
| APC | 4.75x5.5-E | 3 | 11.1 | 12.22 | 135.6 | 18,101 | 94.3 | 283 | 9.98 | 2.09 | |||||
| APC | 5x4.3-E | 3 | 11.1 | 13.60 | 150.9 | 17,657 | 71.9 | 513 | 18.09 | 3.40 | |||||
| APC | 5x4.5-E | 3 | 11.1 | 14.07 | 156.2 | 17,536 | 74.7 | 510 | 17.99 | 3.27 | |||||
| APC | 5x4.6-E | 3 | 11.1 | 14.28 | 158.5 | 17,465 | 76.1 | 541 | 19.09 | 3.42 | |||||
| APC | 5x5-E | 3 | 11.1 | 12.47 | 138.4 | 18,023 | 85.3 | 320 | 11.29 | 2.31 | |||||
| APC | 5.25x4.75-E | 3 | 11.1 | 13.91 | 154.4 | 17,601 | 79.2 | 442 | 15.58 | 2.86 | |||||
| APC | 5.25x6.25-E | 3 | 11.1 | 17.52 | 194.4 | 16,417 | 97.2 | 392 | 13.84 | 2.02 | |||||
| APC | 5.5x4.5-E | 3 | 11.1 | 14.20 | 157.6 | 17,502 | 74.6 | 459 | 16.20 | 2.91 | |||||
| APC | 6x4-E | 3 | 11.1 | 15.73 | 174.6 | 16,992 | 64.4 | 600 | 21.16 | 3.44 | |||||
| APC | 6x4.3-E | 3 | 11.1 | 19.93 | 221.2 | 15,506 | 63.1 | 751 | 26.47 | 3.39 | |||||
| APC | 6x4.5-E | 3 | 11.1 | 19.39 | 215.2 | 15,684 | 66.8 | 758 | 26.73 | 3.52 | |||||
| APC | 6x5.5-E | 3 | 11.1 | 19.38 | 215.2 | 15,703 | 81.8 | 543 | 19.16 | 2.52 | |||||
| APC | 6x6-E | 3 | 11.1 | 19.92 | 221.1 | 15,540 | 88.3 | 610 | 21.53 | 2.76 | |||||
| APC | 7x4-E | 3 | 11.1 | 23.34 | 259.1 | 14,788 | 56.0 | 870 | 30.69 | 3.36 | |||||
| 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 | 4x3.3-E | 4 | 14.8 | 10.15 | 150.2 | 26,188 | 81.8 | 451 | 15.92 | 3.00 | |||||
| APC | 4x4.5-E | 4 | 14.8 | 13.59 | 201.1 | 25,095 | 106.9 | 483 | 17.02 | 2.40 | |||||
| APC | 4.1x4.1-E | 4 | 14.8 | 10.72 | 158.6 | 26,005 | 101.0 | 377 | 13.31 | 2.38 | |||||
| APC | 4.5x4.1-E | 4 | 14.8 | 13.56 | 200.6 | 25,107 | 97.5 | 502 | 17.70 | 2.50 | |||||
| APC | 4.7x4.25-E | 4 | 14.8 | 16.68 | 246.8 | 24,085 | 96.9 | 513 | 18.11 | 2.08 | |||||
| APC | 4.75x4.75-E | 4 | 14.8 | 18.16 | 268.8 | 23,527 | 105.8 | 495 | 17.46 | 1.84 | |||||
| APC | 4.75x5.5-E | 4 | 14.8 | 19.97 | 295.6 | 22,813 | 118.8 | 453 | 15.96 | 1.53 | |||||
| APC | 5x4.3-E | 4 | 14.8 | 21.15 | 313.0 | 21,988 | 89.5 | 803 | 28.31 | 2.56 | |||||
| APC | 5x5-E | 4 | 14.8 | 20.71 | 306.5 | 22,920 | 108.5 | 516 | 18.19 | 1.68 | |||||
| APC | 5.25x4.75-E | 4 | 14.8 | 22.04 | 326.2 | 21,845 | 98.3 | 688 | 24.25 | 2.11 | |||||
| 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. | |||||||||||||||