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Lightning Protection Guidelines for Aerospace VehiclesThis technical memorandum provides lightning protection engineering guidelines and technical procedures used by the George C. Marshall Space Flight Center (MSFC) Electromagnetics and Aerospace Environments Branch for aerospace vehicles. The overviews illustrate the technical support available to project managers, chief engineers, and design engineers to ensure that aerospace vehicles managed by MSFC are adequately protected from direct and indirect effects of lightning. Generic descriptions of the lightning environment and vehicle protection technical processes are presented. More specific aerospace vehicle requirements for lightning protection design, performance, and interface characteristics are available upon request to the MSFC Electromagnetics and Aerospace Environments Branch, mail code EL23.
Document ID
20000004589
Acquisition Source
Marshall Space Flight Center
Document Type
Technical Memorandum (TM)
Authors
Goodloe, C. C.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Date Acquired
September 7, 2013
Publication Date
May 1, 1999
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NASA/TM-1999-209734
M-946
NAS 1.15:209734
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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