The impedance of a rocket-borne capacitive ionospheric probe

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dc.contributor.authorHerman, Jay
dc.date.accessioned2024-04-29T17:00:40Z
dc.date.available2024-04-29T17:00:40Z
dc.date.issued1964-08-01
dc.description.abstractIn a recent paper Herman [1964] obtained an expression for the expected impedance of a capacitive ionospheric probe as a function of electron density N, collision frequency v, temperature T, magnetic field H, and rocket attitude γ with respect to the magnetic field. It was assumed, however, that the magnetic field was along the rocket's axis of symmetry. This restriction is easily removed.
dc.description.urihttps://onlinelibrary.wiley.com/doi/abs/10.1029/JZ069i015p03299
dc.format.extent2 pages
dc.genrejournal articles
dc.identifierdoi:10.13016/m2hawl-ozcn
dc.identifier.citationHerman, J. R. “The Impedance of a Rocket-Borne Capacitive Ionospheric Probe.” Journal of Geophysical Research (1896-1977) 69, no. 15 (1964): 3299–3300. https://doi.org/10.1029/JZ069i015p03299.
dc.identifier.urihttps://doi.org/10.1029/JZ069i015p03299
dc.identifier.urihttp://hdl.handle.net/11603/33352
dc.language.isoen_US
dc.publisherAGU
dc.relation.isAvailableAtThe University of Maryland, Baltimore County (UMBC)
dc.relation.ispartofUMBC Joint Center for Earth Systems Technology (JCET)
dc.relation.ispartofUMBC GESTAR II
dc.rights©2018. American Geophysical Union. All Rights Reserved
dc.titleThe impedance of a rocket-borne capacitive ionospheric probe
dc.typeText
dcterms.creatorhttps://orcid.org/0000-0002-9146-1632

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