| Tempest 1704-2600 Performance Test Data | |||||||||||||||
| Magnets | Motor Wind | Motor Kv | No-Load Current | Motor Resistance | I Max | P Max (3S) | |||||||||
| 12-Pole | 12-Turn Delta | 2600 RPM/Volt | Io = 0.54 Amps @ 10v | Rm = 0.239 Ohms | 9.0 Amps | 100 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 | 0.391 A | 0.445 A | 0.539 A | 0.595 A | 2666 RPM/Volt @ 10v | 0.2387 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 | 4.5x4.1-E | 2 | 7.4 | 5.25 | 38.8 | 14,034 | 54.5 | 156 | 5.49 | 4.00 | |||||
| APC | 4.7x4.25-E | 2 | 7.4 | 5.98 | 44.2 | 13,286 | 53.5 | 156 | 5.49 | 3.52 | |||||
| APC | 4.75x4.75-E | 2 | 7.4 | 6.41 | 47.4 | 12,841 | 57.8 | 152 | 5.36 | 3.20 | |||||
| APC | 4.75x5.5-E | 2 | 7.4 | 7.41 | 54.8 | 12,164 | 63.4 | 131 | 4.61 | 2.39 | |||||
| APC | 5x4.3-E | 2 | 7.4 | 7.54 | 55.8 | 11,548 | 47.0 | 217 | 7.65 | 3.89 | |||||
| APC | 5x4.5-E | 2 | 7.4 | 7.67 | 56.7 | 11,420 | 48.7 | 208 | 7.34 | 3.67 | |||||
| APC | 5x4.6-E | 2 | 7.4 | 7.75 | 57.3 | 11,312 | 49.3 | 224 | 7.91 | 3.91 | |||||
| APC | 5x5-E | 2 | 7.4 | 7.07 | 52.3 | 12,075 | 57.2 | 144 | 5.09 | 2.76 | |||||
| APC | 5.25x4.75-E | 2 | 7.4 | 7.40 | 54.8 | 11,644 | 52.4 | 194 | 6.84 | 3.54 | |||||
| APC | 5.25x6.25-E | 2 | 7.4 | 8.65 | 64.0 | 10,146 | 60.0 | 150 | 5.30 | 2.35 | |||||
| APC | 5.5x4.5-E | 2 | 7.4 | 7.52 | 55.6 | 11,511 | 49.1 | 198 | 6.98 | 3.56 | |||||
| APC | 6x4-E | 2 | 7.4 | 8.00 | 59.2 | 10,948 | 41.5 | 232 | 8.19 | 3.92 | |||||
| APC | 6x4.3-E | 2 | 7.4 | 9.92 | 73.4 | 9,763 | 39.8 | 292 | 10.31 | 3.98 | |||||
| APC | 6x5.5-E | 2 | 7.4 | 9.93 | 73.5 | 9,916 | 51.6 | 213 | 7.50 | 2.89 | |||||
| HQ | 4x4-C | 2 | 7.4 | 4.70 | 34.8 | 14,614 | 55.4 | 161 | 5.66 | 4.62 | |||||
| HQ | 4x4.5-BN | 2 | 7.4 | 5.70 | 42.2 | 13,593 | 57.9 | 177 | 6.24 | 4.20 | |||||
| HQ | 4x4.5-C | 2 | 7.4 | 3.14 | 23.2 | 16,200 | 69.0 | 122 | 4.30 | 5.25 | |||||
| HQ | 5x3-C | 2 | 7.4 | 4.06 | 30.1 | 15,260 | 43.4 | 191 | 6.74 | 6.36 | |||||
| HQ | 5x4-C | 2 | 7.4 | 5.48 | 40.6 | 13,780 | 52.2 | 221 | 7.81 | 5.46 | |||||
| HQ | 5x4.5-BN | 2 | 7.4 | 7.57 | 56.0 | 11,394 | 48.6 | 234 | 8.24 | 4.17 | |||||
| HQ | 5x4.5-C | 2 | 7.4 | 5.60 | 41.4 | 13,661 | 58.2 | 217 | 7.65 | 5.23 | |||||
| HQ | 6x3-C | 2 | 7.4 | 5.53 | 40.9 | 13,750 | 39.1 | 237 | 8.35 | 5.79 | |||||
| HQ | 6x4.5-C | 2 | 7.4 | 8.80 | 65.1 | 10,783 | 46.0 | 291 | 10.25 | 4.46 | |||||
| 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 | 4.5x4.1-E | 3 | 11.1 | 8.73 | 96.9 | 18,375 | 71.3 | 272 | 9.58 | 2.80 | |||||
| APC | 4.7x4.25-E | 3 | 11.1 | 9.86 | 109.5 | 16,710 | 67.3 | 250 | 8.82 | 2.28 | |||||
| HQ | 4x4-C | 3 | 11.1 | 7.71 | 85.6 | 19,691 | 74.6 | 282 | 9.96 | 3.30 | |||||
| HQ | 4x4.5-BN | 3 | 11.1 | 9.25 | 102.7 | 17,548 | 74.8 | 296 | 10.45 | 2.89 | |||||
| HQ | 4x4.5-C | 3 | 11.1 | 5.54 | 61.5 | 22,320 | 95.1 | 233 | 8.20 | 3.78 | |||||
| HQ | 5x3-C | 3 | 11.1 | 6.94 | 77.0 | 20,646 | 58.7 | 345 | 12.18 | 4.48 | |||||
| HQ | 5x4-C | 3 | 11.1 | 8.92 | 99.0 | 17,932 | 67.9 | 368 | 12.98 | 3.72 | |||||
| HQ | 5x4.5-C | 3 | 11.1 | 9.16 | 101.7 | 17,555 | 74.8 | 361 | 12.72 | 3.55 | |||||
| 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. | |||||||||||||||