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Merak-IMU1 Military Optical IMU Inertial Measurement Unit Gyroscope For Missile Guidance

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Merak-IMU1 Military Optical IMU Inertial Measurement Unit Gyroscope For Missile Guidance

MOQ:	1 set
Price:	$1000-$100000
Delivery Period:	30 work days
Payment Method:	T/T
Supply Capacity:	500 sets per year

Details Information

Product Description

Detail Information

Place of Origin

China

Brand Name

Star & Inertia Technology

Model Number

Merak-IMU1

Gyro\Bias Stability (10s):

0.005°/h

Gyro\Zero Bias Stability At Variable Temperature (100s):

0.02°/h

Gyro\Scale Factor Nonlinearity:

≤20ppm

Gyro\Random Walk Coefficient:

0.0005°/½h

Gyro\Input Range:

400°/s

Accelerometer\Zero Bias Repeatability:

Accelerometer\Bias Temperature Sensitivity:

20μg/℃

Accelerometer\Scale Factor Repeatability:

20ppm

Accelerometer\Scale Factor Temperature Sensitivity:

20ppm/℃

Accelerometer\Input:

Features\Operating Temperature:

-40℃～60℃

Features\Storage Temperature:

-45℃～70℃

Features\Power Supply:

18～36V（DC）

Features\Stable Power Consumption:

Features\Mounting Hole Diameter:

4-Φ5.5mm

Features\Dimensions(mm):

130*130*110

Features\Weight:

≤2200g

Highlight:

Military IMU Inertial Measurement Unit

Optical IMU Inertial Measurement Unit

Optical gyroscope measurement units

Product Description

IMU (Merak-IMU1)

This military-grade optical IMU integrates precision gyros and accelerometers in a rugged strapdown architecture. After advanced error compensation processing, it delivers real-time motion data for: • Missile guidance systems • Targeting pods • Stabilization platforms.

Performance advantages:

1) Exceptional accuracy and design adaptability;

2) Solid-state reliability;

3) Instant operation readiness;

4) Optimized SWaP-C characteristics;

5) Extended mission lifespan.

Model			Merak-IMU1
Item	indicator	Description	Parameter
Gyro	Zero bias	Bias stability (10s)	0.005°/h
	Zero bias	Zero bias stability at variable temperature (100s)	0.02°/h
	Scaling Factor	Scale factor nonlinearity	≤20ppm
	Other indicators	Random walk coefficient	0.0005°/½h
	Other indicators	Input range	400°/s
Accelerometer	Deviation	Zero bias repeatability	20μg
	Zero bias	Bias temperature sensitivity	20μg/℃
	Scaling Factor	Scale factor repeatability	20ppm
	Scaling Factor	Scale factor temperature sensitivity	20ppm/℃
	Range indicators	Input range	±20g
Features	Environmental performance	Operating temperature	-40℃～60℃
	Environmental performance	Storage temperature	-45℃～70℃
	General Requirements	Power supply	18～36V(DC)
		Stable power consumption	≤16W
		Mounting hole diameter	4-Φ5.5mm
		Dimensions(mm)	130130110
		Weight	≤2200g

Tags:

Products

MOQ:	1 set
Price:	$1000-$100000
Delivery Period:	30 work days
Payment Method:	T/T
Supply Capacity:	500 sets per year

Detail Information

Product Description

Detail Information

Place of Origin

China

Brand Name

Star & Inertia Technology

Model Number

Merak-IMU1

Gyro\Bias Stability (10s):

0.005°/h

Gyro\Zero Bias Stability At Variable Temperature (100s):

0.02°/h

Gyro\Scale Factor Nonlinearity:

≤20ppm

Gyro\Random Walk Coefficient:

0.0005°/½h

Gyro\Input Range:

400°/s

Accelerometer\Zero Bias Repeatability:

20μg

Accelerometer\Bias Temperature Sensitivity:

20μg/℃

Accelerometer\Scale Factor Repeatability:

20ppm

Accelerometer\Scale Factor Temperature Sensitivity:

20ppm/℃

Accelerometer\Input:

±20g

Features\Operating Temperature:

-40℃～60℃

Features\Storage Temperature:

-45℃～70℃

Features\Power Supply:

18～36V（DC）

Features\Stable Power Consumption:

≤16W

Features\Mounting Hole Diameter:

4-Φ5.5mm

Features\Dimensions(mm):

130*130*110

Features\Weight:

≤2200g

Minimum Order Quantity:

1 set

Price:

$1000-$100000

Delivery Time:

30 work days

Payment Terms:

T/T

Supply Ability:

500 sets per year

Highlight

Military IMU Inertial Measurement Unit

Optical IMU Inertial Measurement Unit

Optical gyroscope measurement units

Product Description

IMU (Merak-IMU1)

Performance advantages:

1) Exceptional accuracy and design adaptability;

2) Solid-state reliability;

3) Instant operation readiness;

4) Optimized SWaP-C characteristics;

5) Extended mission lifespan.

Model			Merak-IMU1
Item	indicator	Description	Parameter
Gyro	Zero bias	Bias stability (10s)	0.005°/h
	Zero bias	Zero bias stability at variable temperature (100s)	0.02°/h
	Scaling Factor	Scale factor nonlinearity	≤20ppm
	Other indicators	Random walk coefficient	0.0005°/½h
	Other indicators	Input range	400°/s
Accelerometer	Deviation	Zero bias repeatability	20μg
	Zero bias	Bias temperature sensitivity	20μg/℃
	Scaling Factor	Scale factor repeatability	20ppm
	Scaling Factor	Scale factor temperature sensitivity	20ppm/℃
	Range indicators	Input range	±20g
Features	Environmental performance	Operating temperature	-40℃～60℃
	Environmental performance	Storage temperature	-45℃～70℃
	General Requirements	Power supply	18～36V(DC)
		Stable power consumption	≤16W
		Mounting hole diameter	4-Φ5.5mm
		Dimensions(mm)	130130110
		Weight	≤2200g

Tags:

Laser Inertial Navigation System

Fiber Optic Inertial Navigation System

Aircraft Inertial Navigation System

Marine Inertial Navigation System

Automotive Inertial Navigation System

AHRS System

IMU Inertial Measurement Unit

Fiber Optic Gyroscope

Ring Laser Gyroscope

Merak-IMU1 Military Optical IMU Inertial Measurement Unit Gyroscope For Missile Guidance

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