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Airplane Engine Piezoelectric Pressure Sensor

Airplane Engine Piezoelectric Pressure Sensor
MPT-t8103
Measuring Range25,60,250 Mpa
Overload≤150%F.S
Sensitivity~100,60,40pC/Mpa
Non-Linearity≤1.0%
Natural Frequency≥150kHz
Rise Time≤4µs
Product Details:

Figuration Drawing

 

 

Technical Data

Measuring Range

2560,250 Mpa

Overload

150%F.S

Sensitivity

100,60,40pC/Mpa

Non-Linearity

1.0%

Natural Frequency

150kHz

Rise Time

4µs

Structure

Water jacket

Shock Resistance

20000g

Signal Output

L5(M5) CONNECTOR

Diameter of Probe

——

Mounting

12pF

Operating Temperature

-25℃~450

Characteristics and Application

Testing of pressure in combustion chamber of diesel engine and airplane engine

 

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