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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

ব্র্যান্ড নাম: Firepower
মডেল নম্বর: এমএফওজি -24
বিস্তারিত তথ্য
উৎপত্তি স্থল:
চীন
সাক্ষ্যদান:
CE, RoHS
সর্বোচ্চ কৌণিক হার:
৫০০ ডিগ্রি/সেকেন্ড
পক্ষপাত স্থায়িত্ব:
1.5 ডিগ্রী/ঘণ্টা
এলোমেলো হাঁটার সহগ:
0.03deg/root-h
জিরো বায়াস পুনরাবৃত্তিযোগ্যতা:
1.5 ডিগ্রী/ঘণ্টা
ব্যান্ড প্রস্থ:
300HZ
সরবরাহ ভোল্টেজ:
+5V
মাত্রা:
24x39 মিমি
ওজন:
30জি
অপারেটিং তাপমাত্রা:
-40C থেকে +65C
স্টোরেজ তাপমাত্রা:
-55C থেকে +85C
বিশেষভাবে তুলে ধরা:

Aerospace Navigation Fiber Optic Gyroscope

,

Satellite Attitude Control FOG Sensor

,

Wide Temperature Range Gyro for Space

পণ্যের বিবরণ
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