Short-circuit currents in three-phase a.c. systems - Factors for the calculation of short-circuit currents according to IEC 60909-0 Ingestion-build-54484 for use in aircraft systems
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Description
for use in aircraft systems at nominal operating pressure of 35 000 kPa (5 080 psi) maximum and temperature range of −54 °C to +135 °C (−65 °F to +275 °F)
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The scope of this document does not include other aspects of ergonomics
Short-circuit currents in three-phase a.c. systems - Factors for the calculation of short-circuit currents according to IEC 60909-0 Ingestion-build-54484 for use in aircraft systems
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