T-Motor AT5230-A Long Shaft Fixed-Wing Motor KV200

T-Motor AT5230-A Long Shaft Fixed-Wing Motor KV200

149,00 €

incl. 19% VAT , plus

AT52 Series Motors suitable for 90E-140E Aircrafts, corresponding to 20-25CC Gasoline Engine

Motor Constant KV

KV200

General

T-Motors AT-Type Electric Motors are especially designed for fixed-wing applications. They have a high temperature resistancy and enable highest flight stability.

Powerful and balanced

Powerful output & Excellent cooling

The design with big torque and heat dissipation structure ensures the powerful flight and good heat dissipation performance

Safety & Long endurance

High temperature (220°C) Military-grade wire improves the high temperature resistance extending the working life time of the motor

High temperature
Working life

Excellent control and balance experience

Throttle linear, strong power and excellent balance ensures various and smooth flights

Strong power
Excellent balance

Durable and strong

High-quality imported bearings, combined with structural strength design ensures toughness for free fly.

Various Mounting Ways

The design with the front and rear shaft can be mounted in the front of or behind firewall of aircraft, both inside or outside of firewall are easy to handle

Manufacturer:
SKU:	187-KV200
GTIN:	4251935113877
Content‍:	1,00 Pieces

Manufacturer information:

T-Motor

http://store-en.tmotor.com/

Specifications:

Test Item: Long Shaft KV200
Motor Dimensions: ø60*122.3mm
Lead: Enameled Wire 100mm
Shaft Diameter:
- IN : 10mm
- OUT : 8mm
Idle Current(10V): 2.7A
Max. Power (180s): 3500W
Weight (Incl. Cable): 610g
Internal Resistance: 22mΩ
Configuration: 24N28P
Rated Voltage (Lipo): 6-12S
Peak Current (180s): 75A
Recommdenation: /

Test Report

Type	Propeller	Throttle	Voltage (V)	Current (A)	Power (W)	RPM	Torque (N x m)	Thrust (g)	Efficiency (g/W)	Operating Temperature (°C)
AT5230-A Long Shaft KV200	FALCON 20-22*10	40%	36.88	5.40	199.02	3032	0.460	1603	8.05	78-102 (Ambient Temperature: /)
		45%	36.84	7.06	260.13	3378	0.561	1987	7.64
		50%	36.78	9.60	353.20	3785	0.685	2488	7.05
		55%	36.70	13.09	480.52	4211	0.837	3091	6.43
		60%	36.63	16.86	617.35	4649	0.999	3750	6.08
		65%	36.56	20.15	736.66	4971	1.131	4263	5.79
		70%	36.45	24.81	904.39	5309	1.295	4918	5.44
		75%	36.35	29.62	1076.71	5656	1.461	5585	5.19
		80%	36.25	34.44	1248.34	5941	1.615	6214	4.98
		90%	36.02	45.45	1637.06	6514	2.089	7553	4.61
		100%	35.77	57.41	2053.49	6793	2.434	8905	4.34
		40%	36.85	6.17	227.25	2993	0.551	1899	8.36
		45%	36.81	8.07	297.08	3321	0.656	2346	7.90
		50%	36.75	11.07	406.83	3716	0.896	2984	7.34
		55%	36.67	14.89	546.11	4119	0.991	3652	6.69
		60%	36.55	19.99	730.83	4567	1.212	4493	6.15
		65%	36.45	24.19	882.01	4875	1.469	5148	5.84
		70%	36.36	29.07	1056.84	5201	1.697	5868	5.55
		75%	36.23	35.04	1269.71	5521	1.898	6707	5.28
		80%	36.13	40.18	1451.84	5798	2.055	7330	5.05
		90%	35.85	53.34	1912.21	6314	2.608	8884	4.65
		100%	36.56	66.54	2366.34	6765	2.977	10167	4.30
		40%	36.84	6.98	257.14	2924	0.666	2212	8.60
		45%	36.78	9.27	340.87	3248	0.785	2733	8.02
		50%	36.70	12.83	470.96	3634	1.041	3463	7.35
		55%	36.61	17.30	633.17	4028	1.205	4210	6.65
		60%	36.48	23.56	859.54	4470	1.479	5212	6.06
		65%	36.39	27.79	1011.32	4753	1.720	5925	5.86
		70%	36.26	33.81	1226.09	5067	1.979	6726	5.49
		75%	36.12	40.68	1469.54	5367	2.216	7649	5.20
		80%	35.99	46.54	1675.26	5624	2.397	8345	4.98
		90%	35.67	61.48	2193.17	6105	2.852	10003	4.56
		100%	35.35	76.51	2704.98	6518	3.339	11500	4.25

Note: Motor temperature is motor surface temperature @100% throttle running 3mins.

(Data above based on benchtest are for reference only, comparison with that of other motor types is not recommended.)

Type	Propeller	Throttle	Voltage (V)	Current (A)	Power (W)	RPM	Torque (N x m)	Thrust (g)	Efficiency (g/W)	Operating Temperature (°C)
AT5230-A Long Shaft KV200	FALCON 18*10	40%	44.27	5.74	254.19	3654	0.496	1681	6.61	83 (Ambient Temperature: /)
		45%	44.23	7.45	329.50	4058	0.599	2079	6.31
		50%	44.15	11.13	491.13	4679	0.751	2760	5.62
		55%	44.07	14.49	638.51	5134	0.932	3315	5.19
		60%	44.00	17.60	774.52	5551	1.089	3898	5.03
		65%	43.94	20.84	915.83	5913	1.227	4453	4.86
		70%	43.84	25.66	1124.70	6340	1.499	5209	4.63
		75%	43.73	30.91	1351.62	6754	1.689	5892	4.36
		80%	43.61	36.43	1588.96	7078	1.850	6249	3.93
		90%	43.36	48.53	2104.20	7736	2.238	7296	3.47
		100%	43.06	62.54	2692.85	8280	2.643	8111	3.01
	FALCON 19*10	40%	44.27	6.12	270.98	3609	0.546	1894	6.99	92 (Ambient Temperature: /)
		45%	44.23	7.99	353.32	4010	0.653	2317	6.56
		50%	44.13	12.47	550.33	4619	0.863	3190	5.80
		55%	44.05	15.71	691.84	5048	1.007	3781	5.47
		60%	43.98	19.51	858.14	5477	1.173	4473	5.21
		65%	43.89	23.39	1026.35	5822	1.318	5069	4.94
		70%	43.78	28.55	1250.05	6249	1.503	5841	4.67
		75%	43.65	34.74	1516.66	6647	1.711	6712	4.43
		80%	43.54	40.31	1755.18	6965	1.895	7455	4.25
		90%	43.26	53.73	2324.24	7599	2.289	8993	3.87
		100%	42.97	67.29	2891.43	8139	2.685	10263	3.55
	FALCON 20*10	40%	44.24	6.89	304.73	3559	0.604	2200	7.22	100 (Ambient Temperature: /)
		45%	44.20	8.93	394.77	3940	0.734	2711	6.87
		50%	44.10	13.71	604.51	4540	0.961	3623	5.99
		55%	44.01	17.55	772.57	4964	1.149	4365	5.65
		60%	43.92	21.86	960.16	5400	1.336	5109	5.32
		65%	44.83	25.89	1139.25	5749	1.501	5784	5.08
		70%	43.72	31.56	1379.72	6145	1.712	6639	4.81
		75%	43.57	38.29	1668.41	6535	1.934	7529	4.51
		80%	43.45	44.35	1926.74	6849	2.137	8337	4.33
		90%	43.13	59.00	2544.65	7462	2.573	10079	3.96
		100%	42.80	74.31	3180.32	7973	2.990	11641	3.66