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ISO 29681 establishes electromagnetic compatibility (EMC) requirements for space systems, covering both conducted and radiated emissions and susceptibility. The standard ensures that spacecraft subsystems do not interfere with each other or with the launch vehicle, and that they survive the electromagnetic environment of launch and orbit.
The standard defines limit curves across the frequency range 20 Hz to 40 GHz. Conducted emissions on power buses are restricted below 60 dBµV from DC to 10 MHz, while radiated emissions are capped at 40 dBµV/m for electric fields above 100 MHz. Susceptibility thresholds require units to withstand 100 V/m from 100 MHz to 18 GHz without performance degradation.
| Phenomenon | Frequency Range | Limit | Test Method |
|---|---|---|---|
| Conducted emission (power) | DC – 10 MHz | ≤ 60 dBµV | CE101 / CE102 |
| Radiated emission (E-field) | 100 MHz – 18 GHz | ≤ 40 dBµV/m | RE102 |
| Radiated susceptibility | 100 MHz – 18 GHz | 100 V/m | RS103 |
| Conducted susceptibility | 30 Hz – 150 kHz | 10 Vrms | CS101 |
Effective EMC design relies on proper grounding (single-point vs. multi-point), twisted-shielded cabling with 360-degree backshell termination, and the strategic placement of bypass capacitors at each unit’s power input. MIL-STD-461 test methods are referenced as the preferred verification approach.