Characterization of Single Event Effect in a Radiation Hardened Programmable Read-Only Memory in a 130 nm Bulk CMOS Technology

被引:0
作者
Yang, Guoqing [1 ]
Zhang, Jizuo [2 ]
Zhang, Jincheng [1 ]
Liu, Xiangyuan [3 ]
Yang, Yimin [2 ]
机构
[1] Xidian Univ, Sch Microelect, Xian 710071, Peoples R China
[2] Guilin Univ Aerosp Technol, Guilin 541004, Peoples R China
[3] Xiangtan Univ, Sch Mat Sci & Engn, Xiangtan 411105, Peoples R China
关键词
PROM; SEU; TID; CHARGE COLLECTION; TOLERANT LATCH; MITIGATION; TAG;
D O I
10.1166/jno.2023.3511
中图分类号
TM [电工技术]; TN [电子技术、通信技术];
学科分类号
0808 ; 0809 ;
摘要
The concept of memory that can only be read but cannot be changed seems strange at first. In reality, it is found that it has great application potential, such as the processor with a fixed purpose, the initial set value of the microprocessor BIOS, and these data are stored in Programmable Read-Only Memory ( PROM) to quickly realize system functions. The PROM storage content is fixed, greatly simplifying his design. The radiation of space particles is the main factor causing the failure of the electronic system of spacecraft. The PROM storage array of the space electronic system is the most basic guarantee for the normal operation of the electronic system. The chip adopts domestic 130 nm standard technology of Complementary Metal Oxide Semiconductor (CMOS), Muller-C digital filter is used in the peripheral subsystem of PROM storage array, and the core cell uses Dual Interlocked Cell (DICE) and ring gate and other radiation hardening technologies to design a 32Kx8bit radiation resistant asynchronous programmable PROM. Pre-silicon of devices was verified by Technology Computer Aided Design (TCAD), and post silicon radiation verification was completed through radiation experiment. The post silicon radiation experiment showed that the total ionizing Dose (TID) capacity of the PROM chip was =100 Krad (Si), the critical value of single event upset (SEU) was =37.1 MeV center dot cm2/mg, the critical value of single event latch up was =98 MeV center dot cm2/mg, meeting the life requirements of the initial value storage of aerospace electronic systems. These performances ensure the reliable operation of the space electronic system after restart.
引用
收藏
页码:1284 / 1295
页数:12
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