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{"title":"No Warm-Up Time Fiber Optic Gyroscope with Wide Dynamic Range Output Mode RS-422","imgUrl":"https:\/\/img.chinax.com\/nimg\/2f\/9d\/c044836c6bc55c8e11ab76da4ba7-200x200-1\/no_warm_up_time_fiber_optic_gyroscope_with_wide_dynamic_range_output_mode_rs_422.jpg","attrs":{"Brand Name":"Firepower","Model Number":"FOG-70-MP","Certification":"CE","Place of Origin":"China"}}
{"title":"High Precision FOG Micro-nano Integrated Fiber Optic Gyroscope with Zero Bias","imgUrl":"https:\/\/img.chinax.com\/nimg\/3e\/c3\/80ec0a8fad96ad5ee1a5a86e7fa4-200x200-1\/high_precision_fog_micro_nano_integrated_fiber_optic_gyroscope_with_zero_bias_stability_e2_89_a40_8_c2_b0_2fh_10s.jpg","attrs":{"Brand Name":"Firepower","Model Number":"MFOG-910A","Certification":"CE","Place of Origin":"Shenzhen, China"}}
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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
Company Details
Bronze Gleitlager
,
Bronze Sleeve Bushings
and
Graphite Plugged Bushings
from Quality China Factory
Business Type:
Manufacturer,Exporter,Trading Company,Seller
Year Established:
2001
Total Annual:
10000000-15000000
Employee Number:
60~100
Ecer Certification:
Verified Supplier
Shenzhen Fire Power Control Technology Co., Ltd. is a professional manufacturer specializing in the production of electronic products and inertial devices, and providing technical consultation and export services. The company has a strong independent team. The technical team is comp... Shenzhen Fire Power Control Technology Co., Ltd. is a professional manufacturer specializing in the production of electronic products and inertial devices, and providing technical consultation and export services. The company has a strong independent team. The technical team is comp...