NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Design guidelines for assessing and controlling spacecraft charging effectsThe need for uniform criteria, or guidelines, to be used in all phases of spacecraft design is discussed. Guidelines were developed for the control of absolute and differential charging of spacecraft surfaces by the lower energy space charged particle environment. Interior charging due to higher energy particles is not considered. A guide to good design practices for assessing and controlling charging effects is presented. Uniform design practices for all space vehicles are outlined.
Document ID
19840025381
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Purvis, C. K.
(NASA Lewis Research Center Cleveland, OH, United States)
Garrett, H. B.
(JPL El Segundo, Calif., United States)
Whittlesey, A. C.
(JPL)
Stevens, N. J.
(Hughes Aircraft Co.)
Date Acquired
September 4, 2013
Publication Date
September 1, 1984
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NAS 1.60:2361
E-2073
NASA-TP-2361
Report Number: NAS 1.60:2361
Report Number: E-2073
Report Number: NASA-TP-2361
Accession Number
84N33452
Funding Number(s)
PROJECT: RTOP 506-55-72
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available