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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

Name: MerakIMU1 Military Optical IMU Inertial Measurement Unit Gyroscope For Missile Guidance
Brand: Star & Inertia Technology
Price: 1000 USD

Brand Name : Star & Inertia Technology

Model Number : Merak-IMU1

Place of Origin : China

MOQ : 1 set

Supply Ability : 500 sets per year

Delivery Time : 30 work days

Price : $1000-$100000

Payment Terms : T/T

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

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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

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

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 Images