X-VSR-SV2 Series

Name: X-VSR-SV2 High Vacuum, Motorized Vertical Stages, Built-in Controllers
Brand: Zaber
SKU: X-VSR-SV2
Availability: InStock

High vacuum vertical stages with built-in controllers

Series Specifications

Download Datasheet

Microstep Size (Default Resolution)	0.09525 µm
Built-in Controller
Repeatability	< 1 µm (< 0.000039")
Loaded Backlash (10 N)	< 10 µm (< 0.000394")
Backlash	< 35 µm (< 0.001378")
Maximum Speed	28 mm/s (1.102"/s)
Minimum Speed	0.000058 mm/s (0.000002"/s)
Speed Resolution	0.000058 mm/s (0.000002"/s)
Peak Thrust	200 N (44.9 lb)
Maximum Continuous Thrust	100 N (22.4 lb)
Communication Interface	RS-232
Communication Protocol	Zaber ASCII (Default), Zaber Binary
Data Cable Connection	Teflon flying leads with M8 4 pin M/F
Maximum Centered Load	100 N (22.4 lb)
Maximum Moment (Pitch)	3 N⋅m (2.2 lb⋅ft)
Maximum Moment (Roll)	3 N⋅m (2.214 lb⋅ft)
Maximum Moment (Yaw)	3 N⋅m (2.214 lb⋅ft)
Pitch	0.08° (1.396 mrad)
Roll	0.08° (1.396 mrad)
Yaw	.08° (1.396 mrad)
Power Supply	24-48 VDC
Power Plug	None, use X-PIB
Maximum Current Draw	950 mA
Linear Motion Per Motor Rev	1.2192 mm (0.048")
Motor Steps Per Rev	200
Motor Type	Stepper (2 phase)
Motor Rated Current	700 mA/phase
Motor Winding Inductance	8.7 mH/phase
Default Resolution	1/64 of a step
Mechanical Drive System	Precision Lead Screw
Limit or Home Sensing	Magnetic home sensor
Manual Control
Axes of Motion	1
Mounting Interface	M6 and M3 threaded holes
Operating Temperature Range	0-50 °C
CE Compliant
Vacuum Compatible	High vacuum (10^-6 Torr)

Part Specifications Comparison

Part Number	Travel Range	Accuracy (unidirectional)	Loaded Accuracy (10 N)	Straightness of Travel	Guide Type	Weight
X-VSR20A-SV2	20 mm (0.787")	50 µm (0.001968")	35 µm (0.001378")	< 30 µm (< 0.001181")	Ball Bearing	0.56 kg (1.235 lb)
X-VSR40A-SV2	40 mm (1.575")	35 µm (0.001378")	20 µm (0.000787")	< 35 µm (< 0.001378")	Crossed-Roller Bearing	0.77 kg (1.698 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

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