The ADIA-2 airborne three - component compensated accelerometer provides measurement of linear accelerations on three mutually - perpendicular axes for airborne flight data recording and processing systems. 

Principle of operation of the ADIA-2 accelerometer - contactless transformation of acting accelerations into electrical signal via magnetoelectric sensor.

SPECIFICATIONS:

1. Axis of measurement.............................. Range, m/s2
   Longitudinal..............................± 20
   Cross-sectional.........................± 20
   Vertical..............................from-30 to + 120
2. Accidental error ±0.5% of range of measurement
3. Systematic error ±0.5% of range of measurement
4. Frequency range of measurement 0-7 Hz
5. Voltage output:at maximum negative accelerationat maximum positive acceleration (0,3±0,2) V(6,1±0,2) V
6. Voltage From 18 up to 31 V (nominal 27 V )
7. Power 5,4 W
8. Mass 0,6 kg
9. Dimensions 90х78х70 mm