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Home Products

Quartz Flexure Accelerometer

Aerospace Navigation Systems High Precision Accelerometer With Temperature Sensor

Name: Aerospace Navigation Systems High Precision Accelerometer With Temperature Sensor
Brand: Shenzhen Fire Power Control Technology Co., LTD
SKU: ZT
Price: 1,250.00 USD
Availability: InStock

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:

Function:

Vibration Test

Operating Voltage:

±（12～18）VDC

Insulation Resistance:

50MΩ，@50VDC

Power Consumption:

≤480mw@±15VDC

Current Consumption:

≤16mA@±15VDC

Weight:

≤80g

Bias:

≤±3 Mg

Scale Factor:

1.25±0.15 MA/g

Packaging Details:

sponge/box

Supply Ability:

500/month

Highlight:

Navigation Systems High Precision Accelerometer

Aerospace High Precision Accelerometer

Temperature Sensor Quartz Flexure Accelerometer

Product Description

Aerospace High-Precision Navigation Systems Accelerometer With Temperature Sensor

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.

Aerospace Navigation Systems High Precision Accelerometer With Temperature Sensor 0

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

Dimension

Aerospace Navigation Systems High Precision Accelerometer With Temperature Sensor 1

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Aerospace Navigation Systems High Precision Accelerometer With Temperature Sensor

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