| Tempest 1704-2050 Performance Test Data | |||||||||||||||
| Magnets | Motor Wind | Motor Kv | No-Load Current | Motor Resistance | I Max | P Max (3S) | |||||||||
| 12-Pole | 16-Turn Delta | 2050 RPM/Volt | Io = 0.34 Amps @ 10v | Rm = 0.325 Ohms | 7.5 Amps | 85 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 | 0.274 A | 0.309 A | 0.341 A | 0.365 A | 2024 RPM/Volt @ 10v | 0.3253 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 | 4.7x4.25-E | 2 | 7.4 | 3.56 | 26.3 | 11,507 | 46.3 | 116 | 4.10 | 4.41 | |||||
| APC | 4.75x4.75-E | 2 | 7.4 | 3.86 | 28.6 | 11,220 | 50.5 | 117 | 4.13 | 4.10 | |||||
| APC | 4.75x5.5-E | 2 | 7.4 | 4.32 | 32.0 | 10,758 | 56.0 | 104 | 3.68 | 3.26 | |||||
| APC | 5x4.3-E | 2 | 7.4 | 4.88 | 36.1 | 10,185 | 41.5 | 171 | 6.02 | 4.73 | |||||
| APC | 5x4.5-E | 2 | 7.4 | 4.93 | 36.4 | 10,150 | 43.3 | 170 | 6.01 | 4.67 | |||||
| APC | 5x4.6-E | 2 | 7.4 | 4.95 | 36.6 | 10,126 | 44.1 | 177 | 6.25 | 4.83 | |||||
| APC | 5x5-E | 2 | 7.4 | 4.38 | 32.4 | 10,695 | 50.6 | 111 | 3.92 | 3.42 | |||||
| APC | 5.25x4.75-E | 2 | 7.4 | 4.70 | 34.8 | 10,348 | 46.5 | 150 | 5.29 | 4.31 | |||||
| APC | 5.25x6.25-E | 2 | 7.4 | 5.65 | 41.8 | 9,375 | 55.5 | 129 | 4.54 | 3.08 | |||||
| APC | 5.5x4.5-E | 2 | 7.4 | 4.76 | 35.2 | 10,294 | 43.9 | 160 | 5.63 | 4.54 | |||||
| APC | 6x4-E | 2 | 7.4 | 5.13 | 38.0 | 9,886 | 37.4 | 191 | 6.72 | 5.02 | |||||
| APC | 6x4.3-E | 2 | 7.4 | 6.26 | 46.3 | 8,698 | 35.4 | 234 | 8.26 | 5.05 | |||||
| APC | 6x4.5-E | 2 | 7.4 | 6.20 | 45.9 | 8,797 | 37.5 | 239 | 8.41 | 5.20 | |||||
| APC | 6x5.5-E | 2 | 7.4 | 6.18 | 45.7 | 8,766 | 45.7 | 167 | 5.89 | 3.65 | |||||
| APC | 6x6-E | 2 | 7.4 | 6.38 | 47.2 | 8,515 | 48.4 | 176 | 6.22 | 3.74 | |||||
| APC | 7x4-E | 2 | 7.4 | 6.60 | 48.8 | 8,245 | 31.2 | 263 | 9.28 | 5.39 | |||||
| APC | 7x4-SF | 2 | 7.4 | 6.61 | 48.9 | 8,224 | 31.2 | 257 | 9.06 | 5.26 | |||||
| APC | 7x5-E | 2 | 7.4 | 7.35 | 54.4 | 7,263 | 34.4 | 223 | 7.87 | 4.10 | |||||
| APC | 7x5-SF | 2 | 7.4 | 7.17 | 53.1 | 7,502 | 35.5 | 244 | 8.62 | 4.60 | |||||
| APC | 7x6-E | 2 | 7.4 | 7.56 | 56.0 | 6,946 | 39.5 | 225 | 7.92 | 4.01 | |||||
| APC | 7x6-SF | 2 | 7.4 | 7.70 | 57.0 | 6,810 | 38.7 | 216 | 7.61 | 3.79 | |||||
| HQ | 5x4.5-BN | 2 | 7.4 | 4.85 | 35.9 | 10,214 | 43.5 | 191 | 6.73 | 5.32 | |||||
| HQ | 5x4.5-C | 2 | 7.4 | 3.31 | 24.5 | 11,760 | 50.1 | 161 | 5.68 | 6.58 | |||||
| HQ | 6x3-C | 2 | 7.4 | 3.33 | 24.6 | 11,844 | 33.6 | 174 | 6.14 | 7.08 | |||||
| HQ | 6x4.5-C | 2 | 7.4 | 5.51 | 40.7 | 9,518 | 40.6 | 227 | 8.02 | 5.58 | |||||
| 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 | 6.26 | 69.4 | 15,401 | 62.0 | 211 | 7.44 | 3.04 | |||||
| APC | 4.75x4.75-E | 3 | 11.1 | 6.68 | 74.1 | 14,875 | 66.9 | 204 | 7.19 | 2.75 | |||||
| APC | 4.75x5.5-E | 3 | 11.1 | 7.23 | 80.3 | 14,076 | 73.3 | 176 | 6.19 | 2.19 | |||||
| APC | 5x5-E | 3 | 11.1 | 7.37 | 81.8 | 13,890 | 65.8 | 191 | 6.73 | 2.33 | |||||
| APC | 5.25x4.75-E | 3 | 11.1 | 7.69 | 85.4 | 13,421 | 60.4 | 255 | 8.99 | 2.99 | |||||
| APC | 5.5x4.5-E | 3 | 11.1 | 7.81 | 86.7 | 13,154 | 56.1 | 262 | 9.24 | 3.02 | |||||
| HQ | 4x4-C | 3 | 11.1 | 4.79 | 53.1 | 17,002 | 64.4 | 215 | 7.57 | 4.04 | |||||
| HQ | 4x4.5-BN | 3 | 11.1 | 5.87 | 65.1 | 15,845 | 67.5 | 239 | 8.43 | 3.67 | |||||
| HQ | 4x4.5-C | 3 | 11.1 | 3.20 | 35.5 | 18,806 | 80.1 | 165 | 5.83 | 4.66 | |||||
| HQ | 5x3-C | 3 | 11.1 | 4.15 | 46.0 | 17,772 | 50.5 | 255 | 8.98 | 5.53 | |||||
| HQ | 5x4-C | 3 | 11.1 | 5.66 | 62.8 | 16,069 | 60.9 | 298 | 10.51 | 4.74 | |||||
| HQ | 5x4.5-BN | 3 | 11.1 | 7.86 | 87.2 | 13,068 | 55.7 | 309 | 10.88 | 3.54 | |||||
| HQ | 5x4.5-C | 3 | 11.1 | 5.78 | 64.2 | 15,900 | 67.8 | 295 | 10.41 | 4.60 | |||||
| HQ | 6x3-C | 3 | 11.1 | 5.64 | 62.5 | 16,050 | 45.6 | 324 | 11.43 | 5.18 | |||||
| HQ | 6x4.5-C | 3 | 11.1 | 8.57 | 95.1 | 11,818 | 50.4 | 358 | 12.62 | 3.76 | |||||
| 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. | |||||||||||||||