Please use this identifier to cite or link to this item: http://nopr.niscair.res.in/handle/123456789/20554
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dc.contributor.authorRajput, S S-
dc.contributor.authorGarg, S C-
dc.date.accessioned2013-08-16T13:42:57Z-
dc.date.available2013-08-16T13:42:57Z-
dc.date.issued2002-10-
dc.identifier.issn0975-1017 (Online); 0971-4588 (Print)-
dc.identifier.urihttp://hdl.handle.net/123456789/20554-
dc.description315-322en_US
dc.description.abstractVarious design considerations and their implementation in an instrument, designed for measurement of electron parameters on-board Indian satellites SROSS-C2, along its orbital path are presented. The proposed instruments measures the electron density in the range 5x102 - 5x106 cm-3 electron temperatures from 500 K to 4000 K, and photoelectron flux of energy 3-30 eV of the order 108 cm- s-1 with full -scale instrument sensitivity 0.2%. Experimental results obtained during testing and flight demonstrate the instrument performance.en_US
dc.language.isoen_USen_US
dc.publisherNISCAIR-CSIR, Indiaen_US
dc.rights CC Attribution-Noncommercial-No Derivative Works 2.5 Indiaen_US
dc.sourceIJEMS Vol.09(5) [October 2002]en_US
dc.titleInstrumentation for a retarding potential analyzer for measurement of electron parametersen_US
dc.typeArticleen_US
Appears in Collections:IJEMS Vol.09(5) [October 2002]

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