The Columbia Model SA-130 is a precision force balance accelerometer developed for the severe shock and vibration environments associated with aircraft and missile flights. This sensor incorporates hi-rel electronic components ensuring long-term stability and superior reliability over a wide temperature range.
The Model SA-130 is light weight and hermetically sealed. Additionally, this unit features a self-test capability requiring an input current range of 0.2 to 3.0 mA/Gdepending on selected operating range. Consult the factory for customized versions of this sensor.
Exports of accelerometers from the United States are subject to the licensing requirements of the Export Administration Regulations (EAR) and/or the International Traffic in Arms Regulations (ITAR).
|Output Impedance||<2000 Ohms|
|Ranges Available||+1 G To +50 G|
|Output Voltage||+5 VDC into 100K Load|
|Excitation||+15 VDC <20 mA|
|Sensitive Axis Alignment||Better Than 0.25 Deg|
|Scale Factor Tolerance||+0.5%|
|Scale Factor Temp Coefficient||0.018% / Deg C Max.|
|Zero Bias||+5 mV or +6 mG (Lower Value Applies)|
|Null Temp Sensitivity||0.00015% F.R./ Deg C|