EMC & Compliance

Avionics EMC

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The electromagnetic compatibility discipline specific to aircraft electronic systems, governed by DO-160 (RTCA) and MIL-STD-461 environmental testing standards. Avionics EMC addresses the unique challenges of aircraft: lightning strike protection, HIRF (High Intensity Radiated Fields) survivability, and coexistence of sensitive navigation receivers with high-power radar and communication transmitters in close proximity.
Category: EMC & Compliance
Standards: DO-160, MIL-STD-461
Unique: Lightning, HIRF, altitude

Comparison

ParameterTypicalHigh-PerfUnitNotes
FrequencyStandardExtendedGHzBand-dependent
PerformanceNominalOptimizeddBApplication-specific
LinearityModerateHighdBcSystem requirement
IntegrationDiscreteMonolithicCost vs performance
CostLowPremium$Volume-dependent

Understanding Avionics EMC

DO-160 Section 20 (Radiated Susceptibility): Field strength up to 200 V/m (7400 V/m for HIRF). DO-160 Section 22 (Lightning): Waveform 1 = 200 kA peak, 6.4 us rise. Pin injection up to 3200V. MIL-STD-461 RE102: Radiated emissions 10 kHz to 18 GHz.
Common Questions

Frequently Asked Questions

How does avionics EMC differ from automotive EMC?

Avionics EMC is more severe in three ways: lightning strike currents (200 kA vs. not applicable in automotive), HIRF exposure from airport surveillance radar (7400 V/m vs. 200 V/m automotive), and altitude derating (reduced cooling and increased arcing risk at 40,000 feet). But automotive has harsher temperature requirements (-40 to +150C vs. -55 to +70C for most avionics).

What is HIRF?

High Intensity Radiated Fields. Aircraft routinely fly through radar beams from airport surveillance radars (ASR-9 at 2.8 GHz, 1.3 MW peak power) and military radars. The resulting field strengths can exceed 7000 V/m. DO-160 Section 20 Category Y tests avionics at these extreme levels.

Why is lightning a major EMC concern for aircraft?

A lightning strike injects 200,000 amperes into the aircraft skin, creating massive magnetic fields and voltage differentials between different parts of the airframe. Current flows through the skin (fuselage acts as a Faraday cage) but couples into wiring harnesses through apertures (windows, seams, antenna holes). Every avionics box must survive these induced transients per DO-160 Section 22.

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