Abstract:The prediction of single event rates depends upon a number of geometrical factors that affect the interpretation of the ground test data and the approach to rate calculations. This paper presents a critical review of these factors. The paper reviews heavy ion rate prediction methods and recommends a standard approach.
“…At the same time, some authors refined expression (4) in order to find the function σ ion (L, θ, ϕ) having in mind the finite thickness of sensitive layer z 0 [38] or the dependence of the SEE cross section on azimuth angle [39]. In addition, it has been found in [40] that for modern VLSIC of dynamic memory with super-large degree of integration (more than 4M) significant deviations from the law σ ion (L, θ, ϕ) = σ(L ef )cosθ may take place.…”
Section: Cross Section Of Single Event Effectsmentioning
confidence: 99%
“…Points represent experimental data[38,39] and curves are the approximations of experimental data by formula(8).…”
Models and methods in use for quantitative estimates of the occurrence of single event upsets in microchips of orbiting spacecraft are considered. A calculation and experimental technique for determining the rate of these effects is described, taking into account spatial and temporal distributions of the fluxes of highenergy particles in the space and their penetration through protective shields. Examples of its application for the orbit of the International Space Station are presented.
Space vehicles (instrumentation modules) used for studying single event inversions of memory cells of RAM VLSIC
SpacecraftCountry of instrumentation design References
“…At the same time, some authors refined expression (4) in order to find the function σ ion (L, θ, ϕ) having in mind the finite thickness of sensitive layer z 0 [38] or the dependence of the SEE cross section on azimuth angle [39]. In addition, it has been found in [40] that for modern VLSIC of dynamic memory with super-large degree of integration (more than 4M) significant deviations from the law σ ion (L, θ, ϕ) = σ(L ef )cosθ may take place.…”
Section: Cross Section Of Single Event Effectsmentioning
confidence: 99%
“…Points represent experimental data[38,39] and curves are the approximations of experimental data by formula(8).…”
Models and methods in use for quantitative estimates of the occurrence of single event upsets in microchips of orbiting spacecraft are considered. A calculation and experimental technique for determining the rate of these effects is described, taking into account spatial and temporal distributions of the fluxes of highenergy particles in the space and their penetration through protective shields. Examples of its application for the orbit of the International Space Station are presented.
Space vehicles (instrumentation modules) used for studying single event inversions of memory cells of RAM VLSIC
SpacecraftCountry of instrumentation design References
IntroductionPredicting the rate of occurrence of single event effects (SEEs) By the early 1990s it was becoming clear that CRÈME and the other early models needed https://ntrs.nasa.gov/search.jsp?R=20120016823 2018-05-12T09:45:40+00:00Z
“…The sensitive volume is used to determine how much energy is deposited from an ion event in a region of interest in a semiconductor device. The methods of obtaining the dimensions of the RPP have been refined and debated since its inception [25][26][27][28][29][30][31], but are typically defined by a combination of theory, technology process information, and experimental analysis. The charge collected from the energy deposited in the SV must be greater or equal to the critical charge of the device for a SEU to be recorded.…”
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