| Tempest 1704-1480 Performance Test Data | |||||||||||||||
| Magnets | Motor Wind | Motor Kv | No-Load Current | Motor Resistance | I Max | P Max (3S) | |||||||||
| 12-Pole | 22-Turn Delta | 1480 RPM/Volt | Io = 0.24 Amps @ 10v | Rm = 0.640 Ohms | 5 Amps | 55 W | |||||||||
| Stator | Outside Diameter | Body Length | Total Shaft Length | Shaft Diameter | Motor Weight | ||||||||||
| 9-Slot | 21.0 mm, 0.827 in. | 15.8 mm, 0.622 in. | 25.5 mm, 1.004 in. | 2.00 mm, 0.079 in. | 14.6 gm, 0.51 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 | 0.204 A | 0.219 A | 0.239 A | 0.248 A | 1467 RPM/Volt @ 10v | 0.6402 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 | 2.31 | 17.1 | 8,025 | 35.0 | 110 | 3.87 | 6.43 | |||||
| APC | 6x4-E | 2 | 7.4 | 2.41 | 17.8 | 7,900 | 29.9 | 119 | 4.20 | 6.67 | |||||
| APC | 6x4.3-E | 2 | 7.4 | 3.05 | 22.5 | 7,105 | 28.9 | 151 | 5.32 | 6.70 | |||||
| APC | 6x4.5-E | 2 | 7.4 | 2.97 | 22.0 | 7,178 | 30.6 | 152 | 5.37 | 6.93 | |||||
| APC | 6x5.5-E | 2 | 7.4 | 3.02 | 22.3 | 7,093 | 36.9 | 105 | 3.72 | 4.72 | |||||
| APC | 6x6-E | 2 | 7.4 | 3.25 | 24.1 | 6,809 | 38.7 | 109 | 3.85 | 4.54 | |||||
| APC | 7x4-E | 2 | 7.4 | 3.24 | 24.0 | 6,819 | 25.8 | 174 | 6.15 | 7.27 | |||||
| APC | 7x4-SF | 2 | 7.4 | 3.24 | 24.0 | 6,814 | 25.8 | 169 | 5.95 | 7.03 | |||||
| APC | 7x5-E | 2 | 7.4 | 3.74 | 27.6 | 6,127 | 29.0 | 154 | 5.43 | 5.57 | |||||
| APC | 7x5-SF | 2 | 7.4 | 3.59 | 26.6 | 6,364 | 30.1 | 166 | 5.86 | 6.25 | |||||
| APC | 7x6-E | 2 | 7.4 | 3.95 | 29.2 | 5,838 | 33.2 | 154 | 5.43 | 5.26 | |||||
| APC | 7x6-SF | 2 | 7.4 | 3.94 | 29.2 | 5,833 | 33.1 | 153 | 5.39 | 5.23 | |||||
| APC | 8x3.8-SF | 2 | 7.4 | 4.04 | 29.9 | 5,680 | 20.4 | 200 | 7.05 | 6.69 | |||||
| APC | 8x4.7-SF | 2 | 7.4 | 4.29 | 31.7 | 5,269 | 23.5 | 200 | 7.06 | 6.31 | |||||
| HQ | 6x4.5-BN | 2 | 7.4 | 3.26 | 24.1 | 6,741 | 28.7 | 152 | 5.35 | 6.29 | |||||
| HQ | 6x4.5-C | 2 | 7.4 | 2.64 | 19.5 | 7,586 | 32.3 | 141 | 4.97 | 7.21 | |||||
| HQ | 7x4.5-C | 2 | 7.4 | 3.62 | 26.8 | 6,294 | 26.8 | 176 | 6.19 | 6.56 | |||||
| 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 | 5x4.3-E | 3 | 11.1 | 3.81 | 42.3 | 10,787 | 43.9 | 185 | 6.54 | 4.38 | |||||
| APC | 5x4.5-E | 3 | 11.1 | 3.79 | 42.1 | 10,819 | 46.1 | 181 | 6.37 | 4.29 | |||||
| APC | 5x4.6-E | 3 | 11.1 | 3.84 | 42.6 | 10,738 | 46.8 | 195 | 6.89 | 4.58 | |||||
| APC | 6x4-E | 3 | 11.1 | 4.04 | 44.9 | 10,376 | 39.3 | 205 | 7.24 | 4.58 | |||||
| APC | 6x5.5-E | 3 | 11.1 | 4.80 | 53.3 | 9,126 | 47.5 | 177 | 6.26 | 3.33 | |||||
| APC | 6x6-E | 3 | 11.1 | 4.94 | 54.8 | 8,836 | 50.2 | 185 | 6.54 | 3.38 | |||||
| HQ | 5x3-C | 3 | 11.1 | 1.87 | 20.7 | 13,688 | 38.9 | 146 | 5.15 | 7.05 | |||||
| HQ | 5x4-C | 3 | 11.1 | 2.60 | 28.8 | 12,553 | 47.5 | 180 | 6.36 | 6.25 | |||||
| HQ | 5x4.5-BN | 3 | 11.1 | 3.79 | 42.0 | 10,796 | 46.0 | 206 | 7.26 | 4.90 | |||||
| HQ | 5x4.5-C | 3 | 11.1 | 2.63 | 29.2 | 12,500 | 53.3 | 176 | 6.22 | 6.04 | |||||
| HQ | 6x3-C | 3 | 11.1 | 2.60 | 28.9 | 12,541 | 35.6 | 188 | 6.65 | 6.52 | |||||
| HQ | 6x4.5-BN | 3 | 11.1 | 5.07 | 56.2 | 8,543 | 36.4 | 242 | 8.53 | 4.30 | |||||
| HQ | 6x4.5-C | 3 | 11.1 | 4.29 | 47.6 | 9,997 | 42.6 | 246 | 8.68 | 5.17 | |||||
| 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. | |||||||||||||||