(Discontinued) LSA-V1 Series

Low vacuum micro motorized linear stages

OVERVIEWFEATURESSPECIFICATIONSSUPPORT & DRAWINGS (PNG, STEP, CAD)

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Series Specifications

Microstep Size (Default Resolution) 0.0238125 µm
Built-in ControllerNo Icon
Recommended Controller X-MCB1 (48 V) Recommended
AutoDetectNo Icon
Repeatability < 1 µm (< 0.000039")
Backlash < 10 µm (< 0.000394")
Maximum Speed 10 mm/s (0.394"/s)
Minimum Speed 0.000015 mm/s (0.000001"/s)
Speed Resolution 0.000015 mm/s (0.000001"/s)
Encoder TypeNo Icon
Peak Thrust 35 N (7.8 lb)
Maximum Continuous Thrust 25 N (5.6 lb)
Vertical Runout < 50 µm (< 0.001968")
Horizontal Runout < 13 µm (< 0.000512")
Linear Motion Per Motor Rev 0.3048 mm (0.012")
Motor Steps Per Rev 200
Motor Type Stepper (2 phase)
Motor Rated Current 240 mA/phase
Motor Winding Resistance 20.4 ohms/phase
Inductance 5 mH/phase
Motor Rated Power 2.35 Watts
Motor Connection Teflon flying leads with D-sub15 connector
Default Resolution 1/64 of a step
Motor Frame Size NEMA 08
Guide Type Ball bearing
Mechanical Drive System Precision lead screw
Limit or Home Sensing Magnetic hall sensor
Axes of Motion 1
Mounting Interface M2 and M3 threaded holes and M4 threaded centre hole
Operating Temperature Range 0 to 50 °C
CE CompliantYes Icon
Vacuum Compatible Low vacuum (10-3 Torr)

Part Specifications Comparison

Part NumberTravel RangeAccuracy (unidirectional)Maximum Centered LoadMaximum Moment (Pitch)Maximum Moment (Roll)Maximum Moment (Yaw)PitchRollYawWeight
LSA10A-V1T4 10 mm (0.394") 18 µm (0.000709") 25 N (5.6 lb) 30 N⋅cm (42.5 oz⋅in) 100 N⋅cm (141.6 oz⋅in) 30 N⋅cm (42.5 oz⋅in) 0.09° (1.570 mrad) 0.03° (0.523 mrad) 0.04° (0.698 mrad) 0.10 kg (0.220 lb)
LSA25A-V1T4 25 mm (0.984") 24 µm (0.000945") 30 N (6.7 lb) 50 N⋅cm (70.8 oz⋅in) 125 N⋅cm (177.0 oz⋅in) 50 N⋅cm (70.8 oz⋅in) 0.14° (2.443 mrad) 0.05° (0.873 mrad) 0.12° (2.094 mrad) 0.14 kg (0.309 lb)

Specification Charts & Notes

Thrust or torque is a function of speed. The values given above are maximums. These values cannot both be achieved simultaneously (i.e. at maximum speed, the unit will not produce maximum thrust).

Thrust Speed Performance

Typical Accuracy