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Accelerometer Gyro Sensor

IMU Accelerometer Gyro

Quartz Flexure Accelerometer

Fiber Optic Gyro

Inertial Navigation System

3 Axis Turntable

Gyro North Finder

Accelerometer Test Equipment

Magnetometer Sensor

1 Axis Turntable

2 Axis Turntable
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home
about us
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quality control
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products

Accelerometer Gyro Sensor

IMU Accelerometer Gyro

Quartz Flexure Accelerometer

Fiber Optic Gyro

Inertial Navigation System

3 Axis Turntable

Gyro North Finder

Accelerometer Test Equipment

Magnetometer Sensor

1 Axis Turntable

2 Axis Turntable
blogs
solutions
contact us
quote

products details

Created with Pixso. Home Created with Pixso. Products Created with Pixso.
Quartz Flexure Accelerometer
Created with Pixso.

Inertial Vibration Sensor Navigation Accelerometer , Flexible Accelerometer For INS

Inertial Vibration Sensor Navigation Accelerometer , Flexible Accelerometer For INS

Inertial Vibration Sensor Navigation Accelerometer , Flexible Accelerometer For INS

Brand Name: Firepower
Model Number: ZT
MOQ: 1
Price: negotiable
Payment Terms: T/T
Supply Ability: 500/month
Detail Information
Product Description
Detail Information
Place of Origin:
China
Certification:
CE
Weight:
≤80g
Bias:
≤±3 Mg
Scale Factor:
1.25±0.15 MA/g
Natural Frequency:
≤800 Hz
Bandwidth:
800～2500
Second-order Nonlinear Coefficient:
≤20 μg /g2
Packaging Details:
sponge/box
Supply Ability:
500/month
Highlight:

Inertial Vibration Sensor Navigation Accelerometer

,

Navigation Flexible Accelerometer

,

INS Flexible Accelerometer

Product Description

Navigation Level Accelerometer Inertial Vibration Sensor Flexible Accelerometer For INS

 

 

 

Performance Characteristics

Electrical properties
Operating voltage ±(12～18)VDC
Insulation resistance 50MΩ,@50VDC
Power consumption ≤480mw@±15VDC
Current consumption ≤16mA@±15VDC

 

Performance Unit
  ZT-01 ZT-02  
Range ≥±30 ≥±30 g
Threshold (resolution) ≤5×10-6g ≤5×10-6g g
Bias ≤±3 ≤±3 mg
Temperature coefficient (-40 ~ 70 ℃) ≤30 ≤35 μg/℃
Monthly composite error (55 ℃, 1σ) ≤30 ≤30 μg
Scale factor 1.25±0.15 1.25±0.15 mA/g
Temperature coefficient (-40 ~ 70 ℃) ≤40 ≤50 ppm/℃
Monthly composite error (55 ℃, 1σ) ≤50 ≤60 ppm
Second-order nonlinear coefficient ≤20 ≤20 μg /g2
Angle of misalignment ≤ 0.48 (100 arcseconds) ≤ 0.48 (100 arcseconds) mrad
Natural frequency ≤800 ≤800 Hz
Bandwidth 800～2500 800～2500 Hz
Operating temperature -45～+80 -45～+80 ℃
Quality ≤80 ≤80 Gram

 

Environmental conditions
Random vibration (unpowered) 8gram, (20～2000) Hz
Shock (without power)

150g,4.5ms,half sine

 

Inertial Vibration Sensor Navigation Accelerometer , Flexible Accelerometer For INS 0

 

Product Introduction

ZT series quartz flexible acceleration sensor is a single-axis torque feedback accelerometer. It detects the external acceleration signal through the detection mass, and then demodulates and amplifies it through the servo circuit. Finally, the output current signal is proportional to the acceleration signal. Products are widely used in aerospace high-precision navigation systems.

 

Dimension

Inertial Vibration Sensor Navigation Accelerometer , Flexible Accelerometer For INS 1

 

Installation requirements

  • The flange surface of the sensor is the installation reference surface.

Precautions

  • The sensor is a wearing part. Please handle it with care and do not drop or touch it. The impact and vibration shall not exceed the technical requirements of the product.
  • The sensor shall be packed reliably during transportation, and there must be no less than 20mm of buffer foam around it, and the sensor shall be fixed with foam. When multiple sensors are packed, ensure that they do not collide with each other.
  • Before power-on, check the wiring of each pin, which shall not be connected incorrectly.
  • The product is stored in the original packaging box in a dry and ventilated environment. Handle with care when moving.
  • Pay attention to electrostatic protection.
Tags: 

Quartz Flexure Accelerometer 1 Axis  

Quartz Flexible Precision Accelerometer  

Navigation High Precision Accelerometer

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