| BadAss BA-2814-1560 Motor Propeller Data | |||||||||||||||
| Magnets | Motor Wind | Motor Kv | No-Load Current | Motor Resistance | I Max | P Max (6S) | |||||||||
| 14-Pole | 10-Turn Delta | 1560 RPM/Volt | Io = 2.93 Amps @ 10v | Rm = 0.020 Ohms | 65 Amps | 1440 W | |||||||||
| Stator | Outside Diameter | Body Length | Total Shaft Length | Shaft Diameter | Motor Weight | ||||||||||
| 12-Slot | 35.6 mm, 1.402 in. | 34.0 mm, 1.339 in. | 55.5 mm, 2.185 in. | 5.00 mm, 0.197 in. | 117 gm, 4.13 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 | 2.712 A | 2.925 A | 3.131 A | 3.333 A | 1518 RPM/Volt @ 10V | 0.0203 Ohms | ||||||||
| 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 | 7x6-E | 3 | 11.1 | 28.26 | 313.7 | 14,734 | 83.7 | 1076 | 37.95 | 3.43 | |||||
| APC | 7x7-E | 3 | 11.1 | 34.29 | 380.6 | 14,313 | 94.9 | 1061 | 37.43 | 2.79 | |||||
| APC | 8x4-E | 3 | 11.1 | 31.83 | 353.3 | 14,475 | 54.8 | 1356 | 47.81 | 3.84 | |||||
| APC | 8x6-E | 3 | 11.1 | 44.57 | 494.7 | 13,569 | 77.1 | 1526 | 53.83 | 3.09 | |||||
| APC | 8x8-E | 3 | 11.1 | 60.38 | 670.2 | 12,368 | 93.7 | 1300 | 45.86 | 1.94 | |||||
| APC | 9x4.5-E | 3 | 11.1 | 44.63 | 495.4 | 13,559 | 57.8 | 1892 | 66.74 | 3.82 | |||||
| APC | 9x6-E | 3 | 11.1 | 50.98 | 565.9 | 13,083 | 74.3 | 1808 | 63.76 | 3.19 | |||||
| APC | 9x7.5-E | 3 | 11.1 | 72.62 | 806.0 | 11,775 | 83.6 | 1803 | 63.58 | 2.24 | |||||
| APC | 10x5-E | 3 | 11.1 | 58.68 | 651.3 | 12,450 | 58.9 | 2164 | 76.34 | 3.32 | |||||
| APC | 10x5.8-F2B | 3 | 11.1 | 62.83 | 697.4 | 11,996 | 65.9 | 2362 | 83.30 | 3.39 | |||||
| APC | 10x6-E | 3 | 11.1 | 63.36 | 703.3 | 12,083 | 68.7 | 2220 | 78.29 | 3.16 | |||||
| APC | 10x7-E | 3 | 11.1 | 72.71 | 807.0 | 11,700 | 77.6 | 2260 | 79.73 | 2.80 | |||||
| MAS | 7x4x3 | 3 | 11.1 | 22.77 | 252.8 | 15,109 | 57.2 | 955 | 33.67 | 3.78 | |||||
| MAS | 8x6x3 | 3 | 11.1 | 44.15 | 490.1 | 13,622 | 77.4 | 1724 | 60.83 | 3.52 | |||||
| MAS | 9x7x3 | 3 | 11.1 | 63.75 | 707.6 | 12,094 | 80.2 | 2253 | 79.48 | 3.18 | |||||
| MAS | 10x5x3 | 3 | 11.1 | 59.55 | 661.0 | 12,502 | 59.2 | 2386 | 84.15 | 3.61 | |||||
| 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 | 6x6-E | 4 | 14.8 | 28.86 | 427.1 | 19,938 | 113.3 | 968 | 34.15 | 2.27 | |||||
| APC | 7x4-E | 4 | 14.8 | 37.67 | 557.5 | 19,274 | 73.0 | 1671 | 58.95 | 3.00 | |||||
| APC | 7x5-E | 4 | 14.8 | 45.82 | 678.1 | 18,635 | 88.2 | 1606 | 56.66 | 2.37 | |||||
| APC | 7x6-E | 4 | 14.8 | 47.33 | 700.4 | 18,521 | 105.2 | 1728 | 60.95 | 2.47 | |||||
| APC | 7x7-E | 4 | 14.8 | 56.29 | 833.1 | 17,787 | 117.9 | 1641 | 57.88 | 1.97 | |||||
| APC | 8x4-E | 4 | 14.8 | 53.93 | 798.2 | 17,923 | 67.9 | 2125 | 74.96 | 2.66 | |||||
| APC | 8x6-E | 4 | 14.8 | 73.21 | 1083.5 | 16,588 | 94.3 | 2316 | 81.69 | 2.14 | |||||
| APC | 9x4.5-E | 4 | 14.8 | 73.51 | 1087.9 | 16,610 | 70.8 | 3004 | 105.97 | 2.76 | |||||
| MAS | 7x4x3 | 4 | 14.8 | 36.28 | 536.9 | 19,371 | 73.4 | 1596 | 56.30 | 2.97 | |||||
| MAS | 8x6x3 | 4 | 14.8 | 68.87 | 1019.3 | 17,067 | 97.0 | 2750 | 97.00 | 2.70 | |||||
| 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 | 5x4.5-E | 5 | 18.5 | 28.90 | 534.6 | 25,833 | 110.1 | 1116 | 39.35 | 2.09 | |||||
| APC | 5x4.6-E | 5 | 18.5 | 28.29 | 523.4 | 25,895 | 112.8 | 1182 | 41.69 | 2.26 | |||||
| APC | 6x4-E | 5 | 18.5 | 33.18 | 613.8 | 25,486 | 96.5 | 1341 | 47.32 | 2.19 | |||||
| APC | 6x4.3E | 5 | 18.5 | 43.44 | 803.7 | 24,597 | 100.2 | 1909 | 67.33 | 2.38 | |||||
| APC | 6x4.5-E | 5 | 18.5 | 40.25 | 744.5 | 24,879 | 106.0 | 1887 | 66.57 | 2.53 | |||||
| APC | 6x5.5-E | 5 | 18.5 | 39.67 | 734.0 | 24,936 | 129.9 | 1411 | 49.76 | 1.92 | |||||
| APC | 6x6-E | 5 | 18.5 | 45.26 | 837.3 | 24,414 | 138.7 | 1440 | 50.78 | 1.72 | |||||
| APC | 7x4-E | 5 | 18.5 | 61.65 | 1140.6 | 22,964 | 87.0 | 2369 | 83.57 | 2.08 | |||||
| APC | 7x5-E | 5 | 18.5 | 68.55 | 1268.2 | 21,875 | 103.6 | 2241 | 79.03 | 1.77 | |||||
| MAS | 7x4x3 | 5 | 18.5 | 55.54 | 1027.4 | 23,507 | 89.0 | 2223 | 78.42 | 2.16 | |||||
| 6-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 | 5x4.3E | 6 | 22.2 | 37.63 | 835.5 | 30,111 | 122.6 | 1524 | 53.76 | 1.82 | |||||
| APC | 5x4.5-E | 6 | 22.2 | 40.99 | 910.0 | 29,881 | 127.3 | 1511 | 53.31 | 1.66 | |||||
| APC | 5x4.6-E | 6 | 22.2 | 39.32 | 873.0 | 29,957 | 130.5 | 1599 | 56.40 | 1.83 | |||||
| APC | 6x4-E | 6 | 22.2 | 45.69 | 1014.4 | 29,401 | 111.4 | 1774 | 62.58 | 1.75 | |||||
| APC | 6x4.3E | 6 | 22.2 | 59.34 | 1317.3 | 28,140 | 114.6 | 2540 | 89.61 | 1.93 | |||||
| APC | 6x4.5-E | 6 | 22.2 | 53.35 | 1184.3 | 28,709 | 122.3 | 2535 | 89.43 | 2.14 | |||||
| APC | 6x5.5-E | 6 | 22.2 | 53.89 | 1196.4 | 28,650 | 149.2 | 1819 | 64.16 | 1.52 | |||||
| APC | 6x6-E | 6 | 22.2 | 60.18 | 1336.0 | 28,081 | 159.6 | 1846 | 65.10 | 1.38 | |||||
| © 2019 Innov8tive Designs, Inc. | |||||||||||||||
| This chart, and the data contained within it, are the property of Innov8tive Designs, Inc., and may not be reproduced without permission from the author. | |||||||||||||||
| 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. | |||||||||||||||