The purpose of this NASA Technical Standard is to establish NASA structural design and test factors, as well as service life factors to be used for spaceflight hardware development and verification. The primary objective of this NASA Technical Standard is to define factors which ensure safe and reliable structural designs. The secondary objective is to reduce space project costs and schedules by enhancing the commonality of use of hardware designs among NASA flight projects, Centers, and their contractors. The criteria in this NASA Technical Standard are to be considered as minimum acceptable values unless adequate engineering risk assessment is provided that justifies the use of lower values. NASA Endorsed. OCE
Electromagnetic compatibility (EMC). Environment-Assessment of the emission levels in the power supply of industrial plants as regards low-frequency conducted disturbances
Electromagnetic compatibility (EMC). Installation and mitigation guidelines-Immunity to HEMP. Specifications for protective devices against HEMP radiated disturbance. Basic EMC publication
Specification for residual current operated circuit-breakers with integral overcurrent protection for household and similar uses (RCCBs)-Applicability of the general rules to RCCBs functionally dependent on line voltage
Residual current operated circuit-breakers with integral overcurrent protection for household and similar uses (RCBOs). Applicablity of the general rules to RCBOs-Applicability of the general rules to RCBOs functionally dependent on line voltage
