BadAss BA-2320-1860 Performance Test Data
	Magnets	Motor Wind		Motor Kv		No-Load Current		Motor Resistance		I Max	P Max (6S)
	14-Pole	7-Turn Delta		1860 RPM/Volt		Io = 2.79 Amps @ 10v		Rm = 0.020 Ohms		55 Amps	1220 W
	Stator	Outside Diameter		Body Length		Total Shaft Length		Shaft Diameter		Motor Weight
	12-Slot	29.1 mm,  1.146 in.		37.6 mm,  1.480 in.		56.0 mm,  2.205 in.		4.00 mm,  0.157 in.		92.5 gm,   3.26 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	2.484 A	2.790 A	3.351 A	3.570 A	1878 RPM/Volt @ 10v		0.0198 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	6x4-E	3	11.1	20.44	226.9	18,905	71.6	730	25.75	3.22
	APC	6x4.3-E	3	11.1	27.84	309.0	18,229	74.2	1027	36.22	3.32
	APC	6x4.5-E	3	11.1	26.65	295.8	18,348	78.2	1014	35.78	3.43
	APC	6x5.5-E	3	11.1	26.84	298.0	18,331	95.5	723	25.51	2.43
	APC	6x6-E	3	11.1	28.28	313.9	18,178	103.3	806	28.43	2.57
	APC	7x4-E	3	11.1	35.05	389.1	17,434	66.0	1327	46.82	3.41
	APC	7x5-E	3	11.1	43.47	482.5	16,714	79.1	1279	45.10	2.65
	APC	7x6-E	3	11.1	44.56	494.7	16,616	94.4	1383	48.78	2.80
	APC	7x7-E	3	11.1	52.79	586.0	15,808	104.8	1309	46.19	2.23
	APC	8x4-E	3	11.1	50.05	555.5	16,107	61.0	1693	59.72	3.05
	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	5x4.3-E	4	14.8	30.46	450.8	25,190	102.6	1057	37.29	2.35
	APC	5x4.5-E	4	14.8	32.19	476.4	24,965	106.4	1047	36.95	2.20
	APC	5x4.6-E	4	14.8	31.46	465.6	25,045	109.1	1119	39.47	2.40
	APC	5x5-E	4	14.8	26.89	397.9	25,522	120.8	630	22.22	1.58
	APC	5.25x4.75-E	4	14.8	30.91	457.5	25,121	113.0	878	30.98	1.92
	APC	5.25x6.25-E	4	14.8	39.55	585.3	24,220	143.3	823	29.03	1.41
	APC	5.5x4.5-E	4	14.8	32.16	475.9	25,006	106.6	929	32.77	1.95
	APC	6x4-E	4	14.8	37.11	549.2	24,490	92.8	1247	44.00	2.27
	APC	6x4.3-E	4	14.8	48.02	710.7	23,345	95.1	1742	61.44	2.45
	APC	6x4.5-E	4	14.8	44.98	665.7	23,683	100.9	1740	61.38	2.61
	APC	6x5.5-E	4	14.8	45.79	677.7	23,632	123.1	1191	42.00	1.76
	APC	6x6-E	4	14.8	49.26	729.0	23,242	132.1	1320	46.57	1.81
	APC	7x4-E	4	14.8	60.24	891.6	21,315	80.7	2041	72.00	2.29
	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	5x4.3-E	5	18.5	44.69	826.7	29,960	122.0	1515	53.43	1.83
	APC	5x4.5-E	5	18.5	48.33	894.0	29,506	125.7	1500	52.91	1.68
	APC	5x4.6-E	5	18.5	46.20	854.8	29,768	129.7	1604	56.57	1.88
	APC	5x5-E	5	18.5	38.45	711.3	30,581	144.8	907	32.00	1.28
	APC	5.25x4.75-E	5	18.5	44.59	824.9	29,895	134.5	1240	43.74	1.50
	APC	5.25x6.25-E	5	18.5	54.57	1009.5	28,746	170.1	1153	40.68	1.14
	APC	5.5x4.5-E	5	18.5	46.01	851.1	29,769	126.9	1330	46.90	1.56
	APC	6x4-E	5	18.5	54.21	1002.9	28,828	109.2	1723	60.77	1.72
	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.