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AZM24AKW-HS50 1.10 in. (28 mm) Direct Connect Stepper Motor with Harmonic Gear (50:1) Web Price Request Quote
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AZM24AKW-HS100 1.10 in. (28 mm) Direct Connect Stepper Motor with Harmonic Gear (100:1) Web Price Request Quote
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AZM24AKW 1.10 in. (28 mm) Direct Connect Stepper Motor Web Price Request Quote
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AZM26AKW 1.10 in. (28 mm) Direct Connect Stepper Motor Web Price Request Quote
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Frame Size | - 1.18 in30 mm | - 1.18 in30 mm | - 1.1 in28 mm | - 1.1 in28 mm | ||||
Motor Length | - 3.11 in.79 mm | - 3.11 in.79 mm | - 2.15 in.54.5 mm | - 2.91 in.74 mm | ||||
Driver Voltage Input Power | - DC | |||||||
Speed-Torque Characteristics |
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Holding Torque |
- 250 oz-in1.8 N·m | - 340 oz-in2.4 N·m | - 13.5 oz-in0.095 N·m | - 26.9 oz-in0.19 N·m | ||||
Shaft/Gear Type | - Harmonic Gear | - Harmonic Gear | - Round Shaft with Flat (No Gearhead) | - Round Shaft with Flat (No Gearhead) | ||||
Gear Ratio (X:1) | - 50 :1 | - 100 :1 | - | - | ||||
Backlash | - | |||||||
Lost Motion | - 1.5 max | - 1.5 max | - | - | ||||
Shaft | - Single | |||||||
Electromagnetic Brake | - Not Equipped | |||||||
Cable Direction | - | |||||||
Permissible Speed Range (r/min) | - 0 ~ 70 | - 0 ~ 35 | - | - | ||||
Rotor Inertia | - 0.066 oz-in²12x10-7 kg·m² | - 0.066 oz-in²12x10-7 kg·m² | - 0.05 oz-in²9.2x10-7 kg·m² | - 0.093 oz-in²17x10-7 kg·m² | ||||
RoHS Compliant |
- These products do not contain substances that exceed the regulation values in the RoHS Directive. | |||||||
Safety Standards |
- CE | |||||||
Permissible Overhung Load | - 0 in. from Shaft End = 22 lb0.2 in. from Shaft End = 30 lb0.39 in. from Shaft End = 39 lb0.59 in. from Shaft End = 56 lb0 mm from Shaft End = 100 N5 mm from Shaft End = 135 N10 mm from Shaft End = 175 N15 mm from Shaft End = 250 N | - 0 in. from Shaft End = 22 lb0.2 in. from Shaft End = 30 lb0.39 in. from Shaft End = 39 lb0.59 in. from Shaft End = 56 lb0 mm from Shaft End = 100 N5 mm from Shaft End = 135 N10 mm from Shaft End = 175 N15 mm from Shaft End = 250 N | - | - | ||||
Permissible Thrust Load | - 31 lb140 N | - 31 lb140 N | - | - | ||||
Permissible Thrust Load | - | |||||||
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