scholarly journals Impact of recombination on heavy ion induced single event upset cross-section

Author(s):  
K S Zemtsov ◽  
A M Galimov ◽  
M E Gorchichko ◽  
I V Elushov
1996 ◽  
Vol 43 (6) ◽  
pp. 2814-2819 ◽  
Author(s):  
L.W. Connell ◽  
F.W. Sexton ◽  
P.J. McDaniel ◽  
A.K. Prinja

2005 ◽  
Vol 52 (6) ◽  
pp. 2125-2131 ◽  
Author(s):  
K.M. Warren ◽  
R.A. Weller ◽  
M.H. Mendenhall ◽  
R.A. Reed ◽  
D.R. Ball ◽  
...  

2021 ◽  
Author(s):  
Li Dong-Qing ◽  
Liu Tian-Qi ◽  
Zhao Pei-Xiong ◽  
Wu Zhen-Yu ◽  
Wang Tie-Shan ◽  
...  

Abstract 3D TCAD simulations demonstrated that reducing the distance between the well boundary and NMOS or PMOS can mitigate the cross section of Single Event Upset (SEU) in 14 nm CMOS bulk FinFET technology. The competition of charge collection between well boundary and sensitive nodes, the enhanced restore currents and the change of bipolar effect are responsible for the decrease of SEU cross section. Different from Dual-interlock cells (DICE) design, under the presence of enough taps to ensure the rapid recovery of well potential, this approach is more effective under heavy ion irradiation of higher LET. Besides, the feasibility of this method and its effectiveness with feature size scaling down are discussed.


2021 ◽  
Vol 120 ◽  
pp. 114128
Author(s):  
Bing Ye ◽  
Li-Hua Mo ◽  
Peng-Fei Zhai ◽  
Li Cai ◽  
Tao Liu ◽  
...  

2007 ◽  
Vol 46 (6A) ◽  
pp. 3377-3379
Author(s):  
Yutaka Arita ◽  
Koji Niita ◽  
Yuji Kihara ◽  
Junich Mitsuhasi ◽  
Mikio Takai ◽  
...  

2011 ◽  
Vol 23 (3) ◽  
pp. 811-816
Author(s):  
姚志斌 Yao Zhibin ◽  
范如玉 Fan Ruyu ◽  
郭红霞 Guo Hongxia ◽  
王忠明 Wang Zhongming ◽  
何宝平 He Baoping ◽  
...  

Symmetry ◽  
2020 ◽  
Vol 12 (12) ◽  
pp. 2030
Author(s):  
Bing Ye ◽  
Li-Hua Mo ◽  
Tao Liu ◽  
You-Mei Sun ◽  
Jie Liu

The on-orbit single-event upset (SEU) rate of nanodevices is closely related to the orbital parameters. In this paper, the on-orbit SEU rate (OOSR) induced by a heavy ion (HI), high-energy proton (HEP) and low-energy proton (LEP) for a 65 nm SRAM device is calculated by using the software SPACE RADIATION under different orbits based on the experimental data. The results indicate that the OOSR induced by the HI, HEP and LEP varies with the orbital parameters. In particular, the orbital height, inclination and shieling thickness are the key parameters that affect the contribution of the LEP to the total OOSR. Our results provide guidance for the selection of nanodevices on different orbits.


2007 ◽  
Vol 54 (6) ◽  
pp. 2303-2311 ◽  
Author(s):  
P. E. Dodd ◽  
J. R. Schwank ◽  
M. R. Shaneyfelt ◽  
J. A. Felix ◽  
P. Paillet ◽  
...  

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