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Single Event Upset Effects on the Clementine Solid State Data Recorder

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dc.contributor.author Garrett, H. B. en_US
dc.contributor.author Johnson, M. S. en_US
dc.contributor.author Ratliff, J. M. en_US
dc.contributor.author Johnson, A. en_US
dc.contributor.author Anderson, S. en_US
dc.contributor.author Stapor, W. J. en_US
dc.date.accessioned 2004-10-03T03:41:15Z
dc.date.available 2004-10-03T03:41:15Z
dc.date.issued 1995-10
dc.identifier.citation AIAA Journal of Spacecraft and Rockets, Special Issue on Clementine, October 1995 en_US
dc.identifier.clearanceno 95-0759
dc.identifier.uri http://hdl.handle.net/2014/30892
dc.description.abstract The sensitivity of the Clementine 2.1 Gbit Solid State Data Recorder (SSDR) to single event upsets was characterized in ground tests. Subsequent in-situ measurements of the ambient radiation environment by experiments on-board Clementine permitted evaluation of the ability of models of the single event phenomenon in the SSDR to be tested using actual data. Initial results from the analysis reveal a nearly constant background upset rate of ~71 bit flips/day for the SSDR. There is no obvious correlation with a solar proton event recorded by Clementine and several other spacecraft on 20-21 February 1994, indicating that the SSDR was not sensitive to protons. The constant rate is thus interpreted as being a function of the Galactic Cosmic Ray heavy ion environment. A pronounced lunar orbit altitude dependence has also been identified in the data though the cause has not yet been unambiguously identified. en_US
dc.format.extent 402807 bytes
dc.format.mimetype application/pdf
dc.language.iso en_US
dc.subject.other Clementine Spacecraft, single event upsets, solid state data recorder en_US
dc.title Single Event Upset Effects on the Clementine Solid State Data Recorder en_US


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