Weight | 8.5 oz |
---|---|
Dimensions | 2.5 × 1.54 × 3.44 in |
Features | • Standard Input Ranges ±2 to ±100 rad/sec² |
Applications | • Aircraft Stability Augmentation |
ASXC Angular Accelerometer
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The Jewell ASXC Series Fluid Rotor Angular Accelerometer is a force balanced servo accelerometer that uses a fluid-filled ring chamber to measure angular acceleration. The ASXC is currently used in a wide variety of applications such as many military and aviation flight controls including autopilot or aircraft stability and control systems or satellite stability.
Additional information
Performance Specifications
Performance Specifications
Performance
Input Range (rad/sec2) | ±2 | ±10 | ±20 | ±50 | ±100 |
Full Range Output (FRO, Volts ±5%) | ±10.0 | ±10.0 | ±10.0 | ±10.0 | ±10.0 |
Non-linearity (%FRO maximum) | 1.0 | 1.0 | 1.0 | 1.0 | 1.0 |
Scale Factor (Volts/rad/sec2, 5%) | 5.000 | 1.000 | 0.500 | 0.200 | 0.100 |
Scale Factor Temperature Sensitivity (% reading/°C maximum) | 0.9 | 0.9 | 0.9 | 0.9 | 0.9 |
Bias (rad/sec2) | ±0.005 | ±0.020 | ±0.030 | ±0.080 | ±0.100 |
Bias Temperature Sensitivity (FRO/°C maximum) | 0.001 | 0.001 | 0.001 | 0.001 | 0.001 |
Natural Frequency (Hz, minimum) | 100 | 150 | 200 | 170 | 170 |
Damping Ratio (nominal) | 0.9 | 0.9 | 0.9 | 0.9 | 0.9 |
Input Axis Misalignment (rad/sec2/rad/sec2, maximum) | ±0.025 | ±0.025 | ±0.025 | ±0.025 | ±0.025 |
Resolution & Threshold (rad/sec2 maximum) | 0.001 | 0.001 | 0.002 | 0.005 | 0.10 |
Electrical
Number of Axes | 1 | ||||
Input Voltage (VDC, 10%) | ±15 | ||||
Input Current (mA nominal) | 25 | ||||
Output Impedance (Ω nominal) | 100 | ||||
Noise (mvrms maximum) | 0.03 | 0.03 | 0.05 | 0.05 | 0.05 |
Environmental
Operating Temperature Range | -30°C to +70°C |
Survival Temperature Range | -40°C to +170°C |
Seal | MIL-STD-202, Method 112 |
Downloads
Downloads
Datasheet |
Outline Drawing |