Accelerometer Sensor

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GSACC202M MEMS Accelerometer with ±2g Range 1000±30 mV/g Sensitivity and ≧ 50 Hz Bandwidth for Aircraft Stability Control

Range: ±2g

Bias: 2.5±0.1 V

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Quartz Flexible Accelerometer Sensor with Wide Load Resistance Range Triangle Precision Mounting Flanges and Bias Stability ≤100μg

Input Range: ±30/40/50/70

Scale Factor: 1000000LSB/g

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GSACC117Q Quartz Flexible Accelerometer Sensor with ±10g Range ≤60ug Bias Stability and 100ug/°C Bias Temperature Sensitivity

Range: ±10g

Bias Repeatability: ≤60ug

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GSACC115Q Quartz Flexible Accelerometer Sensor with ±30g Range 1.0～1.6mA/g Scale Factor and ≤50ug Bias Stability

Range: ±30g

Scale Factor: 1.0～1.6mA/g

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GSACC113Q Quartz Flexible Accelerometer with 0.9～1.3mA/g Scale Factor, 30ug/°C Bias Temperature Sensitivity, and <5mg Bias for Precision Measurement

Range: ±80g

Scale Factor: 0.9～1.3mA/g

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Quartz Flexible Accelerometer Sensor with Ø25.4×29 Size Bias <5mg and Bias Stability ≤10ug for Precision Applications

Scale Factor: 1.2～1.6mA/g

Bias Repeatability: ≤10ug

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GSACC103M MEMS Accelerometer with ±2000 g Range ≤ 5000 Hz Bandwidth and 0.15mV/g Sensitivity

Range: ±2000 G

Bandwidth: ≤ 5000 Hz

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GSACC101M MEMS Accelerometer with ±1 g Range ≥50 Hz Bandwidth and 1000±30 mV/g Sensitivity for Aircraft Stability Control

Input Voltage: 5±0.25 VDC

Input Current: ≤2 MA Output Mode 0.5~4.5V

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KSIMU008C Inertial Navigation System Specification

Power Dissipation: ≤20W

Dimension: 110×110×100mm

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KSIMU005M Three Axis Quartz IMU MEMS Accelerometer Sensor

Input Voltage: 5±0.2 V DC

Input Current: ≤100mA

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Quartz acceleration sensors for microgravity measurement devices with Threshold ≤1 (μg) and Resolution ≤1 (μg)

Bias: ≤5mg

Input Voltage: ±12 ~ ±18(V)

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Quartz accelerometers for vibration detection with Bias ≤5mg and Bias One-month Composite Repeatability ≤30(μg)

Input Voltage: ±12 ~ ±18(V)

Bias Temperature Sensitivity: ≤30(μg/℃)

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Shock 100g and Threshold 1 μg Accelerometer Sensor with Linearity ≤10 μg/g2

Scale Factor One-month Composite Repeatability: ≤10 (1σ) (10-6)

Scale Factor Temperature Sensitivity: ≤10 (10-6/℃)

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High precision quartz accelerometers for inertial navigation systems with Bias≤5mg

Operating Temperature: -45 ~ +80(℃)

Input Voltage: ±12 ~ ±18(V)

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High-performance Vibration Monitoring with Accelerometer Detector Ф25.4mm X30mm

Power Supply: 12V-15V

Deviation Value K0/K1: ≤±3 Mg

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Quartz accelerometers for satellite control units with Bias ≤5mg and Range =±20g

Linearity: ≤10 (μg/g2)

Scale Factor Temperature Sensitivity: ≤10 (ppm/℃)

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