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.
Notes:
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 |
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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 |