Specification for Dipole Magnetic Shield Generator (DMSG Module)

1. Objective
   • To design and construct a dipole magnetic shield capable of generating a controlled magnetic field to deflect charged particles or reduce external magnetic interference, suitable for use in spacecraft radiation shielding or sensitive experimental environments.
2. General Description
   • The dipole magnetic shield generates a magnetic field with a dipolar configuration, achieving a specified field intensity and uniformity. The shield is designed for high efficiency, durability, and compatibility with the operational environment (e.g., space or laboratory).
3. Technical Specifications
   1. Magnetic Field Requirements:
      • Field Intensity: Adjustable between 1 Gauss (0.1 mT) to 10,000 Gauss (1 T).
      • Field Uniformity: Within ±5% in the specified operational zone.
      • Field Shape: Dipolar configuration with adjustable orientation.
      • Field Stability: Fluctuation < 0.01% over 24 hours.
   2. Operational Zone:
      • Volume Coverage: Cylindrical zone with dimensions: Diameter 1.0 m, Length 2.0 m.
      • Shielding Effectiveness: Reduction of external field interference by 90% within the operational zone.
   3. Material and Construction:
      • Core Material: High-permeability alloys (e.g., Mu-metal) for guiding magnetic flux.
      • Coil Type: Superconducting or copper-wound solenoids depending on application.
      • Coil Cooling:
        • Superconducting coils: Cryogenic cooling with liquid helium or closed-loop refrigeration.
        • Copper coils: Forced-air or liquid cooling.
      • Encapsulation: Non-magnetic, high-strength composite materials for structural support.
   4. Power Supply and Control:
      • Input Voltage: 110V/220V AC or 24V DC (configurable).
      • Current Requirements: Adjustable up to 200A depending on field intensity.
      • Control System:
        • Digital interface with real-time monitoring.
        • Programmable field intensity and polarity.
        • Remote operation capability via Ethernet or wireless.
   5. Thermal Management:
      • Heat Dissipation: Active thermal management with thermal sensors and redundant cooling mechanisms.
      • Operating Temperature Range: -50°C to 60°C (ambient).
   6. Environmental Durability:
      • Radiation Hardness: Withstands ionizing radiation up to 100 krad.
      • Withstands Static magnetic fields: Requires shielding with high magnetic permeability materials like permalloy, mu-metal, or nanocrystalline grain structure ferromagnetic metal coatings.
      • Low-frequency magnetic fields (ELF): 300 Hz to 3 kHz, requires shielding with materials like steel or stainless steel.
      • Radiofrequency (RF) electromagnetic radiation: Requires shielding with conductive materials like copper, brass, nickel, silver, steel, or tin.
      • Extremely low frequency (ELF) electromagnetic radiation: 3 Hz to 300 Hz, requires shielding with materials like steel or stainless steel.
      • Optical radiation: Includes visible and near-ultraviolet electromagnetic radiation, which may induce photochemical reactions or accelerate radical reactions.
      • Vibration Resistance: Operates under vibration up to 20g (space-rated).
      • Vacuum Compatibility: All materials and components suitable for high vacuum (10^-6 Torr).
4. Performance Metrics
   • Magnetic Field Precision:
     • Field alignment accuracy: ±1 degree.
     • Response time to change settings: < 0.1 seconds.
   • Energy Efficiency: Power consumption under 5 kW at maximum field intensity.
   • Lifetime: Minimum 10 years with less than 5% degradation in performance.
5. Integration Requirements
   • Structural Interface: Mounting points compatible with standard spacecraft or laboratory platforms.
   • Electrical Interface: Standardized connectors and interface protocols (e.g., RS-485, CAN bus).
   • Safety Features:
     • Automatic shutdown in case of overheating or current overload.
     • Shielding of stray magnetic fields to prevent interference with nearby equipment.
6. Testing and Validation
   • Factory Acceptance Test (FAT):
     • Verify field intensity, uniformity, and stability.
     • Measure thermal performance and cooling efficiency.
   • Site Acceptance Test (SAT):
     • Confirm functionality in operational environment.
     • Validate integration with external systems.
   • Endurance Test: Continuous operation for 1000 hours under maximum field settings.
7. Documentation and Deliverables
   • Full technical drawings and 3D CAD models.
   • Operation and Maintenance Manual (OMM).
   • Test Reports from FAT and SAT.
   • Compliance Certificates (e.g., ISO 9001, space certification).
8. Applicable Standards
   • IEC 61000 for electromagnetic compatibility.
   • NASA or ESA standards for space-rated components.
   • ANSI/ASME standards for mechanical construction.
9. Additional Notes
   • Optional features like automated alignment systems and additional shielding layers can be provided upon request.
   • Adaptations for specific environments (e.g., underwater or extreme temperatures) are available on a custom basis.