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Aerospace Fiber Optic Gyroscope MFOG-24 with ≤0.03°/√h ARW Wide Temperature Range -40°C to +65°C and Compact φ24*39mm Design

Name: Aerospace Fiber Optic Gyroscope MFOG-24 with ≤0.03°/√h ARW Wide Temperature Range -40°C to +65°C and Compact φ24*39mm Design
Brand: Shenzhen Fire Power Control Technology Co., LTD
SKU: MFOG-24
Price: 10000 USD
Availability: InStock

Brand Name:	Firepower
Model Number:	MFOG-24

Detail Information

Product Description

Detail Information

Place of Origin:

China

Certification:

CE, RoHS

Maximum Angular Rate:

500deg/s

Bias Stability:

1.5deg/h

Random Walk Coefficient:

0.03deg/root-h

Zero Bias Repeatability:

1.5deg/h

Band Width:

300Hz

Supply Voltage:

+5V

Dimensions:

24x39mm

Weight:

30g

Operating Temperature:

-40C To +65C

Storage Temperature:

-55C To +85C

Highlight:

Aerospace Navigation Fiber Optic Gyroscope

Satellite Attitude Control FOG Sensor

Wide Temperature Range Gyro for Space

Product Description

Aerospace Fiber Optic Gyroscope MFOG-24 Wide Temperature Range ≤0.03°/√h ARW for Satellite Attitude Control Systems

The MFOG-24 is an aerospace-grade fiber optic gyroscope engineered for satellite attitude control systems and spacecraft navigation. Delivering exceptional ≤0.03°/√h angular random walk and ≤1.5°/h bias stability across a wide -40°C to +65°C operating temperature range, this solid-state gyroscope provides reliable inertial measurement for LEO satellites, CubeSats, launch vehicles, and deep-space probes. Its compact φ24*39mm design and ≤30g weight are optimized for the stringent mass and volume constraints of aerospace missions.

Key Features for Aerospace Applications

Angular random walk ≤0.03°/√h delivers ultra-low noise for precision star tracker and reaction wheel integration
Bias stability ≤1.5°/h ensures accurate attitude determination during orbital maneuvers
Wide operating temperature -40°C~+65°C handles thermal cycling in LEO satellite environments
Storage temperature -55°C~+85°C survives launch vehicle environmental extremes
±500°/s measurement range covers high-rate spacecraft slewing and despinning
No moving parts eliminates mechanical failure risk in vacuum environment
≤1.5W ultra-low power consumption compatible with satellite power budget constraints
Fast initialization enables rapid attitude acquisition after deployment

Aerospace and Satellite Application Scenarios

LEO Satellite Attitude Determination: Provides high-accuracy angular rate data for three-axis stabilized Earth observation and communication satellites, integrated with star trackers and sun sensors.
CubeSat and SmallSat Navigation: Ultra-compact φ24*39mm form factor fits within 1U and 3U CubeSat chassis for academic, commercial, and defense small satellite missions.
Launch Vehicle Guidance: Delivers reliable angular rate feedback during ascent, stage separation, and orbital insertion phases of small and medium-lift launch vehicles.
Re-Entry Vehicle Control: Maintains accurate attitude reference through atmospheric re-entry conditions for sample return capsules and spaceplanes.

Technical Specifications

Parameter	MFOG-24
Measurement Range	±500°/s
Bias Stability	≤1.5°/h
Angular Random Walk	≤0.03°/√h
Zero-Bias Repeatability	≤1.5°/h
Bandwidth (3dB)	≥300Hz
Power Supply	5V ±0.15
Power Consumption	≤1.5W
Operating Temperature	-40°C~+65°C
Storage Temperature	-55°C~+85°C
Vibration Resistance	20g, 20-2000Hz
Dimensions	φ24*39mm
Weight	≤30g
Moving Parts	None

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products details

Aerospace Fiber Optic Gyroscope MFOG-24 with ≤0.03°/√h ARW Wide Temperature Range -40°C to +65°C and Compact φ24*39mm Design

Aerospace Fiber Optic Gyroscope MFOG-24 with ≤0.03°/√h ARW Wide Temperature Range -40°C to +65°C and Compact φ24*39mm Design

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