Design and Selection Criteria of High Temperature Accelerometers for Aerospace Propulsion

Accelerometers and pressure sensors for measurement in aerospace propulsion systems require special consideration during design and manufacturing processes.

Specialized applications frequently require use of a single sensor model, which must be capable of operating over significantly wider temperature ranges, for example, -420 to +1300 °F (-251 to +705 °C), while providing high accuracy, stability and reliability.

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