LC40C-KM04 Series
Belt-driven T-slot cantilever axis with stepper motors, for external controllers
Series Specifications
Part Specifications Comparison
Showing 18 of 18 Parts.
| Part Number | Travel Range | Moving Mass | Maximum Axial Brake Force | Weight |
|---|---|---|---|---|
| LC40C0100-KM04 | 100 mm (3.937") | 1.01 kg (2.222 lbs) | 1.947 kg (4.292 lb) | |
| LC40C0100-KM04B | 100 mm (3.937") | 1.01 kg (2.222 lbs) | 70 N (15.7 lb) | 1.947 kg (4.292 lb) |
| LC40C0150-KM04 | 150 mm (5.905") | 1.13 kg (2.486 lbs) | 2.066 kg (4.555 lb) | |
| LC40C0150-KM04B | 150 mm (5.905") | 1.13 kg (2.486 lbs) | 70 N (15.7 lb) | 2.066 kg (4.555 lb) |
| LC40C0200-KM04 | 200 mm (7.874") | 1.25 kg (2.750 lbs) | 2.186 kg (4.819 lb) | |
| LC40C0200-KM04B | 200 mm (7.874") | 1.25 kg (2.750 lbs) | 70 N (15.7 lb) | 2.186 kg (4.819 lb) |
| LC40C0250-KM04 | 250 mm (9.843") | 1.37 kg (3.014 lbs) | 2.186 kg (4.819 lb) | |
| LC40C0250-KM04B | 250 mm (9.843") | 1.37 kg (3.014 lbs) | 70 N (15.7 lb) | 2.186 kg (4.819 lb) |
| LC40C0300-KM04 | 300 mm (11.811") | 1.49 kg (3.278 lbs) | 2.424 kg (5.344 lb) | |
| LC40C0300-KM04B | 300 mm (11.811") | 1.49 kg (3.278 lbs) | 70 N (15.7 lb) | 2.424 kg (5.344 lb) |
| LC40C0350-KM04 | 350 mm (13.780") | 1.61 kg (3.542 lbs) | 2.544 kg (5.609 lb) | |
| LC40C0350-KM04B | 350 mm (13.780") | 1.61 kg (3.542 lbs) | 70 N (15.7 lb) | 2.544 kg (5.609 lb) |
| LC40C0400-KM04 | 400 mm (15.748") | 1.73 kg (3.806 lbs) | 2.663 kg (5.871 lb) | |
| LC40C0400-KM04B | 400 mm (15.748") | 1.73 kg (3.806 lbs) | 70 N (15.7 lb) | 2.663 kg (5.871 lb) |
| LC40C0450-KM04 | 450 mm (17.716") | 1.85 kg (4.070 lbs) | 2.783 kg (6.135 lb) | |
| LC40C0450-KM04B | 450 mm (17.716") | 1.85 kg (4.070 lbs) | 70 N (15.7 lb) | 2.783 kg (6.135 lb) |
| LC40C0500-KM04 | 500 mm (19.685") | 1.97 kg (4.334 lbs) | 2.902 kg (6.398 lb) | |
| LC40C0500-KM04B | 500 mm (19.685") | 1.97 kg (4.334 lbs) | 70 N (15.7 lb) | 2.902 kg (6.398 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).
