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Electrical Bonding for NASA Launch Vehicles, Spacecraft, Payloads, and Flight Equipment

Options for Standards Update Notification System (SUNS)
Send SUNS Updates
Yes
SUNS Notification Type
Correction
Organization that Developed the Standard
Organization that Developed the Standard
NASA Standard
Document Identifiers
Document Number
NASA-STD-4003
Version
A w/CHANGE 1
Change Number
1
Document Date
Change Date
Is Active?
ACTIVE
NASA Organization and Technical Discipline
Responsible NASA Organization
NASA HQ, Office, Facility or Division
NASA HQ Office, Facility or Division
OCE - Office of the Chief Engineer
Technical Discipline Category
4000 - Electrical and Electronics Systems, Avionics/Control Systems, Optics
Endorsed Standard
Endorsement Details
Endorsing NASA Organization
OCE Endorsed Standard
NASA Core Standard
No
NASA Endorsement Date
NASA Endorsed Standard Status
NASA Endorsed Standard
Mandatory Standard
NASA Mandatory Standard
Not a NASA Mandatory Standard
Document Scope
Document Scope
The purpose of this Standard is to define the basic electrical bonding requirements for NASA launch vehicles, spacecraft, payloads, and equipment. Its intent is to provide fundamental aerospace electrical bonding requirements, as well as to classify electrical bonds according to their purpose. This Standard also 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.
Keywords
Electrical Bonding for NASA Launch Vehicles, Spacecraft, Payloads, and Flight Equipment
Document Access Control
Document Viewable by
Export Control/Distribution Authorization
Internet Public -- Standard is cleared for public accessibility on the internet.
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PUBLIC: Document History for Standard
nasa-std-4003.pdf (112.13 KB)
nasa-std-4003a.pdf (331.92 KB)
Important Standard Dates
Next 5-Year Review Date
Revalidated or Reaffirmed Date

 


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