Dytran model 3533A is a triaxial, IEPE, accelerometer with TEDS capabilities used in aerospace flight testing, Health and Usage Monitoring Systems (HUMS), and commercial and military aircraft vibration monitoring.
Dytran model 3533A is a triaxial, IEPE, accelerometer with TEDS capabilities used in aerospace flight testing, Health and Usage Monitoring Systems (HUMS), and commercial and military aircraft vibration monitoring.
File |
Description |
Type |
Languages |
---|---|---|---|
3533A Vibration Transducer | Technical Document | English |
Type/technology | Piezoelectric CCLD (IEPE) |
Direction/Axes | Triaxial |
Measurement range [m/s²] | 10000 m/s² |
Measurement range [g] | 1000 g |
Application | General purpose |
Weight [gram] | 28 g |
Weight [oz] | 0.99 oz |
Sensitivity tolerance | 5 % |
Sensitivity | 5 mV/g |
Lower frequency [Hz] | 3.3 Hz |
Higher frequency [Hz] | 1 kHz |
Minimum Temperature [°C] | -50 °C |
Maximum Temperature [°C] | 120 °C |
Minimum Temperature [°F] | -60 °F |
Maximum Temperature [°F] | 250 °F |
Mounting | Stud mounting |
Resonance frequency [kHz] | 50 kHz |
Real-time capabilities | None |
Electric isolation | None |
Output signal (connectivity) | Analogue |
Electrical connector location | Side |
TEDS | No |
Filtering | None |