NASA-STD-4003
ELECTRICAL BONDING FOR NASA LAUNCH VEHICLES, SPACECRAFT, PAYLOADS, AND FLIGHT EQUIPMENT
| Organization: | NASA |
| Publication Date: | 8 September 2003 |
| Status: | inactive |
| Page Count: | 25 |
scope:
This standard defines the basic electrical bonding requirements for NASA launch vehicles, spacecraft, payloads, and equipment.
Purpose. The intent of this standard is to provide fundamental aerospace electrical bonding requirements. This standard classifies electrical bonds according to their purpose and states the requirements for the various classes. The rationale for specific requirements is stated where possible. Additional data is provided to support tailoring for new applications if necessary.
Applicability. This Standard recommends engineering practices for NASA programs and projects. It may be cited in contracts and program documents as a technical requirement or as a reference for guidance. Determining the suitability of this Standard and its provisions is the responsibility of program/project management and the performing organization. Individual provisions of this standard may be tailored (i.e. modified or deleted) by contract or program specifications to meet specific program/project needs and contraints.
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