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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

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

نام تجاری: Firepower
شماره مدل: MFOG-24
اطلاعات دقیق
محل منبع:
چین
گواهی:
CE, RoHS
حداکثر نرخ زاویه ای:
500 درجه بر ثانیه
ثبات تعصب:
1.5 درجه در ساعت
ضریب راه رفتن تصادفی:
0.03 درجه/ریشه ساعت
تکرارپذیری سوگیری صفر:
1.5 درجه در ساعت
عرض باند:
300 هرتز
ولتاژ تغذیه:
+ 5 ولت
ابعاد:
24x39mm
وزن:
30 گرم
دمای عملیاتی:
-40 تا +65 درجه سانتیگراد
دمای ذخیره سازی:
-55C تا +85C
برجسته کردن:

Aerospace Navigation Fiber Optic Gyroscope

,

Satellite Attitude Control FOG Sensor

,

Wide Temperature Range Gyro for Space

توضیح محصول
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