(Discontinued) T-LS Series

Motorized linear stages with built-in controllers

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Series Specifications

Microstep Size (Default Resolution) 0.09921875 µm
Built-in ControllerYes Icon
Accuracy (unidirectional) 29 µm (0.001142")
Repeatability < 2 µm (< 0.000079")
Backlash < 14 µm (< 0.000551")
Maximum Speed 6.5 mm/s (0.256"/s)
Minimum Speed 0.000930 mm/s (0.000037"/s)
Speed Resolution 0.000930 mm/s (0.000037"/s)
Encoder TypeNo Icon
Peak Thrust 32 N (7.2 lb)
Maximum Continuous Thrust 15 N (3.4 lb)
Communication Interface RS-232
Communication Protocol Zaber Binary
Data Cable Connection Minidin 6
Maximum Centered Load 100 N (22.4 lb)
Maximum Moment (Transverse) 125 N⋅cm (177.0 oz⋅in)
Power Supply 12-16 VDC
Power Plug 2.1 mm centre positive
Maximum Current Draw 300 mA
Linear Motion Per Motor Rev 0.6096 mm (0.024")
Motor Steps Per Rev 48
Motor Type Stepper (2 phase)
Inductance 60 mH/phase
Default Resolution 1/128 of a step
Guide Type Ball bearing
Mechanical Drive System Precision lead screw
Limit or Home Sensing Magnetic home sensor
Axes of Motion 1
LED IndicatorsYes Icon
Stage Parallelism < 100 µm (< 0.003937")
Operating Temperature Range 0 to 50 °C
CE CompliantYes Icon
Vacuum CompatibleNo Icon

Part Specifications Comparison

Part NumberTravel RangeManual ControlMounting InterfaceWeight
T-LS13E 13 mm (0.512")Yes Icon 1/4"-20 0.57 kg (1.257 lb)
T-LS13E-S 13 mm (0.512")No Icon 1/4"-20 0.57 kg (1.257 lb)
T-LS13M 13 mm (0.512")Yes Icon M6 0.57 kg (1.257 lb)
T-LS13M-S 13 mm (0.512")No Icon M6 0.57 kg (1.257 lb)
T-LS28E 28 mm (1.102")Yes Icon 1/4"-20 0.59 kg (1.301 lb)
T-LS28E-S 28 mm (1.102")No Icon 1/4"-20 0.59 kg (1.301 lb)
T-LS28M 28 mm (1.102")Yes Icon M6 0.59 kg (1.301 lb)
T-LS28M-S 28 mm (1.102")No Icon M6 0.59 kg (1.301 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

When powering multiple units from an unregulated power supply, the voltage and thus the available thrust will be reduced. To achieve the thrust specified above, each unit should have its own power supply.