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High Temperature Blade Crack Propagation


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Description

The High Temperature, High Speed Disk/Blade Crack Propagation Test System was specifically designed for NASA to develop new techniques for crack detection of turbine blades and disks.

  • Operates up to 10,000 RPM at 1000° F
  • The entire assembly is mounted to a cast aluminum base plate fitted with stiffeners.
  • Install and operate the machine on a sturdy surface for best operation.