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Electrically Isolating Thermally Coupled Device for Noise Suppression of Circuits in Deep SpaceMixed mode rad hard avionics Systems on a Chip (SoC) designed for deep space applications such as Europa orbiters and Europa Landers will require data isolation circuits to block noise. This paper presents the simulation performance for a novel rad hard SOI CMOS compatible thermal transducer used for on-chip data isolation in SoC. The research presented involves the use of commercially available computer aided design tools to model the transient electrothermal behavior of the transducer. Both one- and two-dimensional analyses of a prototype thermal transducer were performed. Results indicate that thermal-based data isolator technology can pass a data bit in under a microsecond and, as a measurement of feasibility, I(exp 2)C bus specifications can be met.
Document ID
20010041257
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
Authors
Mantooth, A.
(Arkansas Univ. Fayetteville, AR United States)
McNutt, T.
(Arkansas Univ. Fayetteville, AR United States)
Mojarradi, M.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA United States)
Li, H.
(Idaho Univ. Moscow, ID United States)
Blalock, B.
(Mississippi State Univ. Mississippi State, MS United States)
Date Acquired
August 20, 2013
Publication Date
January 1, 2001
Publication Information
Publication: Forum on Innovative Approaches to Outer Planetary Exploration 2001-2020
Subject Category
Lunar And Planetary Science And Exploration
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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