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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Negotiable
MOQ:
Negotiable
Delivery Time:
Negotiable
Brand:
Firepower
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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Company
Shenzhen Fire Power Control Technology Co., LTD
Location
429, Building A10, Fuhai Information Port, Xinhe Community, Fuhai Street, Shenzhen, Guangdong, China
Contact Person
Caine