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Electromagnetic Effects Testing

Product Specifications

̽»¨ÊÓÆµ is equipped to perform electromagnetic environmental effects (E3) testing to meet our customer needs while accommodating government, military (all branches) and commercial aircraft specifications. ̽»¨ÊÓÆµ engineers located in Greenville, Texas are experienced in E3/TEMPEST design and testing of aircrafts units and systems with certifications that include NARTE Electromagnetic Control Engineer and NSA TEMPEST Engineer. ̽»¨ÊÓÆµ meets customer requirements by conducting electromagnetic effects design and electromagnetic interference (EMI) screen room testing to RTCA DO-160 and MIL STD 461 which provides system level risk mitigation as well as aircraft FAA supplemental type certification (STC) approvals.

  •  Strict Adherence to Control of EMI
  •  Safety Issues: Aircraft Safe to Fly with Respect to EMC
  •  Reduction of Interference to Avionics
  •  Radiation Hazards
  •  Communications Security
  •  Electromagnetic Pulse (EMP)
  • EME Analysis 
  • Identify Potential Incompatibilities Early (Protection is Designed Into the System)
  • High Intensity Radiated Fields (HIRF)
  • Lightning Analysis
  • Precipitation Static Analysis
  • Design Support 
  • Define Shielding and Grounding Schemes
  • Define Red/Black Architecture for Secure Systems
  • Define Wire Categories for Interface Cable Routing
  • Define Electrical Bonding Requirements
  • Define Lightning Protection
  • Installation & Integration Support
  • Hazards of Electromagnetic Radiation to Ordinance (HERO)
  • Hazards of Electromagnetic Radiation to Fuels (HERF)
  • Hazards of Electromagnetic Radiation to Personnel (HERP)
  • Antenna Radome Transmissivity Testing
  • MIL STD-461/ RTCA DO-160 
  • Conducted Emissions
  • Radiated Emissions
  • Conducted Susceptibility
  • Radiated Susceptibility
  • Capabilities for Group B EMI Testing

TEMPEST Evaluations
Equipment Level Evaluations

RTCA DO-160G as defined below: 

  • Section 16.0 Power Input, Category A Equipment
  • Section 17.0 Voltage Spike, Category A Equipment
  • Section 18.0 Audio Frequency Conducted
  • Susceptibility - Power Inputs; Category R Equipment
  • Section 19.0 Induced Signal Susceptibility (Radiated and Conducted); Category CC Equipment
  • Section 20.0 Radio Frequency Susceptibility (Radiated and Conducted); Category R Equipment (Note 1)
  • Section 21.0 Emission of Radio Frequency Energy; Category M Equipment

MIL-STD-461F as defined below: 

  • CE102 Conduced Emissions, Power Leads, 10 kHz to 10 MHz
  • CS101 Conducted Susceptibility, Power Leads, 30Hz to 150 kHz
  • CS114 Conducted Susceptibility, Bulk Cable Injection, 10 kHz to 200 MHz, Curve 3
  • CS115 Conducted Susceptibility, Bulk Cable Injection, Impulse Excitation
  • CS116 Conducted Susceptibility, Damped Sinusoidal Transients, Cables and Power Leads,10 kHz to 100 MHz
  • RE102 Radiated Emissions, Electric Field, 2 MHz to 18 GHz
  • RS103 Radiated Susceptibility, Electric Field, 2 MHz to 18 GHz (Note 2)

Notes:
(1) Maximum radiated susceptibility field level from 400 MHz to 8 GHzis 60 V\m
(2) Air Force Aircraft Internal field levels up to a maximum frequency of 8 GHz

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