Presentation 1995/9/22
The On-Orbit Measurement of Single Event Upset by ETS-VI Satellite
Tateo GOKA, Haruhisa MATSUMOTO, Masayuki HIGUCHI, Takashi HADA,
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Abstract(in Japanese) (See Japanese page)
Abstract(in English) The space parts are required high reliability and radiation hardness. Especially memory devices and microprocessors are required immunity from Single Event Upset(SEU). The SEU is one major problem of 3 major spacecraft anomalies by space environments. SEU in-flight measurements are presented on 2 radiation hardened microelectronics, 64kb SRAMs, 8bit microprocessors ( 4kgates gate-array ) in the ETS-VI satellite orbit(8000km-38000km , 13 degrees inclination ). SEU rate prediction using CREME code and ground-testing data are compared
Keyword(in Japanese) (See Japanese page)
Keyword(in English) SEU / Space Part / Radiation Hardness / Soft Error / Gate Array / Memory Device
Paper # R95-10
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Committee R
Conference Date 1995/9/22(1days)
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Registration To Reliability(R)
Language JPN
Title (in Japanese) (See Japanese page)
Sub Title (in Japanese) (See Japanese page)
Title (in English) The On-Orbit Measurement of Single Event Upset by ETS-VI Satellite
Sub Title (in English)
Keyword(1) SEU
Keyword(2) Space Part
Keyword(3) Radiation Hardness
Keyword(4) Soft Error
Keyword(5) Gate Array
Keyword(6) Memory Device
1st Author's Name Tateo GOKA
1st Author's Affiliation Office of Reserch and Development, NASDA()
2nd Author's Name Haruhisa MATSUMOTO
2nd Author's Affiliation Office of Reserch and Development, NASDA
3rd Author's Name Masayuki HIGUCHI
3rd Author's Affiliation Office of Reserch and Development, NASDA
4th Author's Name Takashi HADA
4th Author's Affiliation Office of Reserch and Development, NASDA
Date 1995/9/22
Paper # R95-10
Volume (vol) vol.95
Number (no) 257
Page pp.pp.-
#Pages 6
Date of Issue