Liquid Propellant Rocket Engine Inspection System


Production inspection of regenerative cooled thrust chambers, nozzle and assemblies

Designed for fast and accurate nondestructive inspection of structures, components and repairs.

Powerful defect analysis tools

Easily programmable image processing macros in LaserNDT 1.8.0 Software Suite for improved operator image analysis and reporting.

Versatile camera

Easily mounts to scan gantries, robots, crawlers, tripods, vacuum attachments, and customer defined test configurations.

Test configuration

All Mode Operation: Thermal, Vacuum, Vibration and Pressure Stressing.


Test Part Stressing Systems, Test Chambers, Gantries, Workstations, and Robotic Scanners.

Views and Configurations


System includes

Shear camera with a built-in 100 mw laser light source (Class IIIa), image processing computer, interconnect cables, tripod, transit case and Operator and Applications Manual

Optional equipment

Thermal Stress Systems TES-50 (500W) or TES-200 (2kW) with software control and adjustable radiant beam spread.

Table Mount, remote control Pan & Tilt, MQTT Robot Integration Software

Shear Camera Dimensions

12.0 x 4.0 x 5.5 in / 30.5 x 10.2 x 14.0 cm

Shear Camera

6.2 lbs. / 2.8 kg


1628 x 1236 12 bit/30 fps


100 to 240 VAC, 50/60 Hz20 amps maximum (with TES-200)

Operation Modes

Shearography testing with Thermal, Ultra Sonic or Accustic Vibration, Vacuum or Mechanical test part stressing Analysis and Measurement• Defect Location on test part• Image Integration and Z axis measurement

Shear Vector

Fully adjustable Shear Vector: 0-360 ?/0-10 ?

Image Calibration

Manual and Auto Cal., real-time readout of FOV, Scale, Shear Vector

Laser Light Source

100 mw, Class IIIa Laser Product

System Software

LaserNDT 1.8.0


Patents: The LTI-2100 is manufactured in the USA under US and foreign patents 6,717,68; 5,257,088; 5,094,528. Additional patents pending. Specifications are subject to change.

Laser Shearography Certifications AIA NAS 410, ASNT SNT-TC-1A, ASTM E2581-07, EN 4179

LTI-2100 inspection of composite aircraft structures on the hangar floor.

Inspection Applications
Shearography in Action

Shearography detects: Delaminations, Disbonds, Impact damage, Repair defects, Porosity, Cracks ,Fiber waves or wrinkles

Disbonds in metal braze bonded coolantchannels. Field of View = 10 x 12 in.
Non-visible impact damage on a carbon fiber laminate aircraft wing panel. Field of View = 8 x 8 in.
COPV fiber bridging defects.Tank diameter = 6.4 in.

Our Full Line of Shearography NDT Systems

Shearography can be applied to many applications, if we don't have a system that works for you, we can custom build one that will.

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Tirpod, Gantry Scanner Or Robot Mounting

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Compact Digital Shearography System

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Shearography NDT System for Ciritcal Aerospace Components

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Portable Thermal Laser Shearography

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Large Chamber Shearography System

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Liquid Propellant Rocket Engine Inspection System

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Digital Holography Inspection System

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Get the help you need

Custom NDT Solutions