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INS IMU Navigation Vibration Sensor , Inertial Quartz Flexure Accelerometer

INS IMU Navigation Vibration Sensor , Inertial Quartz Flexure Accelerometer

Brand Name:	Firepower
Model Number:	JB11
MOQ:	1
Price:	negotiable
Payment Terms:	T/T
Supply Ability:	500/month

Detail Information

Product Description

Detail Information

Place of Origin:

China

Certification:

Function:

Vibration Test

Bias K0/K1:

≤±3mg

Threshold:

5μg

Scale Factor K1:

1.05~1.30 MA/g

Second Order Nonlinearity Coefficient K2:

≤±10μg /g2

Weight:

≤80g

Packaging Details:

sponge/box

Supply Ability:

500/month

Highlight:

INS Navigation Vibration Sensor

IMU Quartz Flexure Accelerometer

Acceleration Transducer For INS IMU

Product Description

INS IMU Navigation Vibration Sensor, Inertial Quartz Flexure Accelerometer

Product Overview

The quartz flexible accelerometer is a high-precision military inertial navigation grade accelerometer with exceptional long-term stability, repeatability, start-up performance, environmental adaptability, and reliability. Suitable for both static and dynamic testing, it serves as a standard vibration sensor.

The product's output current maintains a linear relationship with the applied force or acceleration. Users can select appropriate sampling resistors to achieve high-precision output. An optional built-in temperature sensor enables compensation of offset values and scale factors to minimize environmental temperature effects.

Key Specifications

Attribute	Value
Function	vibration test
Bias K0/K1	≤±3mg
Threshold	5μg
Scale factor K1	1.05~1.30 mA/g
Second order nonlinearity coefficient K2	≤±10μg /g2
Weight	≤80g

Product Image

Performance Characteristics

No.	Parameters	JB01-1	JB01-02	JB01-03
1	Range	±50g	±50g	±50g
2	Threshold	5μg	5μg	5μg
3	Bias K0/K1	≤±3mg	≤±3mg	≤±5 mg
4	Scale factor K1	1.05~1.30 mA/g	1.05~1.30 mA/g	1.05~1.30 mA/g
5	Second order nonlinearity coefficient K2	≤±10μg /g2	≤±15μg /g2	≤±20μg /g2
6	0g 4 hours short-term stability	≤10 μg	≤15 μg	≤20 μg
7	1g 4 hours short-term stability	≤10 ppm	≤15 ppm	≤20 ppm
8	Bias comprehensive repeatability σK0 (1σ,1 month)	≤10 μg	≤20 μg	≤30 μg
9	Scale factor comprehensive repeatability σK1/K1 (1σ,1 month)	≤15ppm	≤30 ppm	≤50 ppm
10	Nonlinearity coefficient comprehensive repeatability K2/K1(1σ, 1 month)	≤±10 μg /g2	≤±20 μg /g2	≤±30 μg /g2
11	Bias thermal coefficient (full temp. mean)	≤±10 μg /℃	≤±30 μg /℃	≤±50 μg /℃
12	Scale factor thermal coefficient (full temp. mean)	≤±10 ppm /℃	≤±30 ppm /℃	≤±50 ppm /℃
13	Noise (sampling resistance 840Ω)	≤5mv	≤8.4mv	≤8.4mv
14	Natural frequency	400~800 Hz	400~800 Hz	400~800 Hz
15	Bandwidth	800~2500 Hz	800~2500 Hz	800~2500 Hz
16	Random vibration	6g(20-2000Hz)	6g(20-2000Hz)	6g(20-2000Hz)
17	Impact	100g,5ms,1/2sin	100g,5ms,1/2sin	100g,5ms,1/2sin
18	Working temp.	-55~+85℃	-55~+85℃	-55~+85℃
19	Store temp.	-60~+120℃	-60~+120℃	-60~+120℃
20	Power supply	±12~±15V	±12~±15V	±12~±15V
21	Consume current	≤±20mA	≤±20mA	≤±20mA
22	Thermal sensor	Customizable	Customizable	Customizable
23	Size	Ф25.4X30mm	Ф25.4X30mm	Ф25.4X30mm
24	Weight	≤80g	≤80g	≤80g

Applications

Drilling Inclination Measurement
Aeronautics Astronautics
Instruments Inertial Equipment

Key Features

High resolution
High stability
High accuracy
Low power consumption
Excellent overload capacity
Compact size
Cost-effective
Broad measurement range

Product Dimensions

Documentation

Product Documentation

Tags:

Accelerometer Gyro Sensor

IMU Accelerometer Gyro

Quartz Flexure Accelerometer

Fiber Optic Gyro

Inertial Navigation System

Gyro North Finder

Magnetometer Sensor

Accelerometer Gyro Sensor

IMU Accelerometer Gyro

Quartz Flexure Accelerometer

Fiber Optic Gyro

Inertial Navigation System

Gyro North Finder

Magnetometer Sensor

products details

INS IMU Navigation Vibration Sensor , Inertial Quartz Flexure Accelerometer

INS IMU Navigation Vibration Sensor , Inertial Quartz Flexure Accelerometer

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