| Tempest 1708-1700 Performance Test Data | |||||||||||||||
| Magnets | Motor Wind | Motor Kv | No-Load Current | Motor Resistance | I Max | P Max (3S) | |||||||||
| 12-Pole | 9-Turn Delta | 1700 RPM/Volt | Io = 0.55 Amps @ 10v | Rm = 0.236 Ohms | 10 Amps | 110 W | |||||||||
| Stator | Outside Diameter | Body Length | Total Shaft Length | Shaft Diameter | Motor Weight | ||||||||||
| 9-Slot | 21.0 mm, 0.827 in. | 19.5 mm, 0.768 in. | 29.5 mm, 1.161 in. | 2.00 mm, 0.079 in. | 21.2 gm, 0.75 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 | 0.433 A | 0.497 A | 0.546 A | 0.596 A | 1796 RPM/Volt @ 10v | 0.1531 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 | 4.92 | 36.4 | 10,571 | 46.0 | 194 | 6.84 | 5.32 | |||||
| APC | 5.25x4.75-E | 2 | 7.4 | 4.64 | 34.3 | 10,775 | 48.5 | 162 | 5.71 | 4.72 | |||||
| APC | 5.25x6.25-E | 2 | 7.4 | 5.99 | 44.3 | 9,970 | 59.0 | 147 | 5.19 | 3.32 | |||||
| APC | 5.5x4.5-E | 2 | 7.4 | 4.80 | 35.5 | 10,675 | 45.5 | 173 | 6.11 | 4.88 | |||||
| APC | 6x4-E | 2 | 7.4 | 5.23 | 38.7 | 10,415 | 39.5 | 211 | 7.43 | 5.44 | |||||
| APC | 6x4.3-E | 2 | 7.4 | 6.70 | 49.6 | 9,556 | 38.9 | 276 | 9.72 | 5.56 | |||||
| APC | 6x4.5-E | 2 | 7.4 | 6.61 | 48.9 | 9,628 | 41.0 | 279 | 9.85 | 5.71 | |||||
| APC | 6x5.5-E | 2 | 7.4 | 6.57 | 48.6 | 9,588 | 49.9 | 199 | 7.03 | 4.10 | |||||
| APC | 6x6-E | 2 | 7.4 | 6.78 | 50.1 | 9,474 | 53.8 | 218 | 7.69 | 4.35 | |||||
| APC | 7x4-E | 2 | 7.4 | 7.34 | 54.3 | 9,148 | 34.7 | 324 | 11.43 | 5.96 | |||||
| APC | 7x4-SF | 2 | 7.4 | 7.39 | 54.7 | 9,110 | 34.5 | 316 | 11.16 | 5.78 | |||||
| APC | 7x5-E | 2 | 7.4 | 8.45 | 62.5 | 8,400 | 39.8 | 299 | 10.56 | 4.79 | |||||
| APC | 7x5-SF | 2 | 7.4 | 8.26 | 61.1 | 8,542 | 40.4 | 313 | 11.05 | 5.13 | |||||
| APC | 7x6-E | 2 | 7.4 | 8.92 | 66.0 | 8,094 | 46.0 | 305 | 10.75 | 4.62 | |||||
| APC | 7x6-SF | 2 | 7.4 | 9.16 | 67.7 | 7,896 | 44.9 | 289 | 10.20 | 4.27 | |||||
| APC | 8x3.8-SF | 2 | 7.4 | 9.52 | 70.4 | 7,569 | 27.2 | 384 | 13.56 | 5.46 | |||||
| APC | 8x4.7-SF | 2 | 7.4 | 10.04 | 74.3 | 7,134 | 31.8 | 383 | 13.51 | 5.16 | |||||
| HQ | 5x4.5-BN | 2 | 7.4 | 4.86 | 35.9 | 10,643 | 45.4 | 207 | 7.29 | 5.75 | |||||
| HQ | 6x4.5-BN | 2 | 7.4 | 7.31 | 54.1 | 9,154 | 39.0 | 284 | 10.01 | 5.25 | |||||
| HQ | 6x4.5-C | 2 | 7.4 | 5.73 | 42.4 | 10,123 | 43.1 | 259 | 9.15 | 6.12 | |||||
| HQ | 7x4.5-C | 2 | 7.4 | 8.18 | 60.5 | 8,593 | 36.6 | 332 | 11.72 | 5.49 | |||||
| 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 | 4.1x4.1-E | 3 | 11.1 | 4.64 | 51.5 | 17,044 | 66.2 | 163 | 5.76 | 3.17 | |||||
| APC | 4.5x4.1-E | 3 | 11.1 | 5.39 | 59.9 | 16,560 | 64.3 | 216 | 7.62 | 3.61 | |||||
| APC | 4.7x4.25-E | 3 | 11.1 | 6.26 | 69.5 | 15,977 | 64.3 | 226 | 7.96 | 3.25 | |||||
| APC | 4.75x4.75-E | 3 | 11.1 | 6.81 | 75.6 | 15,595 | 70.1 | 219 | 7.74 | 2.90 | |||||
| APC | 4.75x5.5-E | 3 | 11.1 | 7.52 | 83.5 | 15,071 | 78.5 | 200 | 7.06 | 2.40 | |||||
| APC | 5x4.3-E | 3 | 11.1 | 8.26 | 91.7 | 14,536 | 59.2 | 345 | 12.17 | 3.76 | |||||
| APC | 5x4.5-E | 3 | 11.1 | 8.39 | 93.1 | 14,419 | 61.4 | 338 | 11.94 | 3.63 | |||||
| APC | 5x4.6-E | 3 | 11.1 | 8.48 | 94.2 | 14,364 | 62.6 | 361 | 12.72 | 3.83 | |||||
| APC | 5x5-E | 3 | 11.1 | 7.62 | 84.6 | 14,981 | 70.9 | 222 | 7.82 | 2.62 | |||||
| APC | 5.5x4.5-E | 3 | 11.1 | 8.42 | 93.5 | 14,409 | 61.4 | 312 | 11.00 | 3.34 | |||||
| APC | 6x4-E | 3 | 11.1 | 9.02 | 100.1 | 13,961 | 52.9 | 391 | 13.79 | 3.91 | |||||
| APC | 6x5.5-E | 3 | 11.1 | 11.22 | 124.6 | 12,925 | 67.3 | 362 | 12.75 | 2.90 | |||||
| HQ | 5x3-C | 3 | 11.1 | 3.89 | 43.2 | 17,551 | 49.9 | 247 | 8.72 | 5.72 | |||||
| HQ | 5x4-C | 3 | 11.1 | 5.54 | 61.5 | 16,445 | 62.3 | 312 | 10.99 | 5.06 | |||||
| HQ | 5x4.5-BN | 3 | 11.1 | 8.42 | 93.5 | 14,425 | 61.5 | 374 | 13.19 | 4.00 | |||||
| HQ | 5x4.5-C | 3 | 11.1 | 5.69 | 63.2 | 16,375 | 69.8 | 312 | 10.99 | 4.93 | |||||
| HQ | 6x3-C | 3 | 11.1 | 5.52 | 61.3 | 16,460 | 46.8 | 340 | 12.00 | 5.55 | |||||
| HQ | 6x4.5-C | 3 | 11.1 | 9.57 | 106.2 | 13,502 | 57.5 | 459 | 16.20 | 4.33 | |||||
| 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. | |||||||||||||||