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NASA-STD-4003A, NASA TECHNICAL STANDARD: ELECTRICAL BONDING FOR NASA LAUNCH VEHICLES, SPACECRAFT, PAYLOADS, AND FLIGHT EQUIPMENT (05-FEB-2013)

NASA-STD-4003A, NASA TECHNICAL STANDARD: ELECTRICAL BONDING FOR NASA LAUNCH VEHICLES, SPACECRAFT, PAYLOADS, AND FLIGHT EQUIPMENT (05-FEB-2013)., This Standard is published by the National Aeronautics and Space Administration (NASA) to provide uniform engineering and technical requirements for processes, procedures, practices, and methods that have been endorsed as standard for NASA programs and projects, including requirements for selection, application, and design criteria of an item. This Standard is approved for use by NASA Headquarters and NASA Centers, including Component Facilities and Technical and Service Support Centers. This Standard establishes a common framework for consistent electrical bonding practices across NASA programs. The intent is to provide stand-alone requirements and to provide enough data to help modify requirements or to allow waivers if needed.

NASA-STD-4003 Rev. A

    
 Status:
Active

 FSC Code:
 1810 - Space Vehicles

Version:
A02-2013330.25 KB NASA-STD-4003A
09-2003151.56 KB NASA-STD-4003

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