MC3232, Landing Gear Sensor
The MC3232 force/torque sensor was designed for use in research, development, and testing of aircraft landing gear equipment. The MC3232 instrument is particularly suitable for applications requiring simultaneous multi-axis measurement of...
Features:
- Specifically designed for measurement of aircraft landing gear tire impact forces
- Commonly used to provide continuous measurement of all the Fx, Fy, and Fz forces during drop testing of landing gear mechanisms
- Body of the load cell is manufactured from high-strength aluminum with mounting provisions on the top and bottom surfaces
Manufacturer: Advanced Mechanical Technology Inc. (AMTI)
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Description
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MC3232 - Description
The MC3232 force/torque sensor was designed for use in research, development, and testing of aircraft landing gear equipment. The MC3232 instrument is particularly suitable for applications requiring simultaneous multi-axis measurement of several large forces and moments, or measurements of large forces that change direction and position over time.
MC3232 - Specifications
| Type | Multi-Axis |
| # of Axis | 6 (Fx, Fy, Fz, Mx, My, Mz) |
| Full Scale | 50000 lbs |
| Precision | ±0.02 % FS |
| Min Temperature | -18 °C |
| Max Temperature | 52 °C |
MC3232 - Downloads
MC3232 Force Torque Sensor Datasheet |
MC3232 - Similar Products
- Designed for measurement of aircraft landing gear tire impact forces
- Measure forces during drop testing of landing gear mechanisms
- Low mass top plate; provides high vertical and horizontal natural frequencies
| Type | Multi-Axis |
| # of Axis | 3 (Fz, Mx, My) |
| Full Scale | 100000 lbs, 150000 lbs, 200000 lbs |
| Precision | ±0.02 % FS |
| Min Temperature | -18 °C |
| Max Temperature | 52 °C |