In advanced technology, static random-access memory (SRAM) cells used in space are highly sensitive to charge variations caused by high-energy particle strikes, which cause soft-error. Therefore, it is imperative for an SRAM to withstand this harsh environment. However, 6T cells are unable to function reliably in such a place. In order to address this, a radiation-hardened readdecoupled 12T (RHRD12T) SRAM cell is proposed in this paper. The relative strength of RHRD12T is estimated by comparing it with other contemporary cells such as NS10T, PS10T, RHBD10T, QUATRO12T, QUCCE12T, and RHD12T on various major design metrics. Due to the read-decoupled nature of RHRD12T, it shows the highest read stability. It also consumes the lowest hold power compared to all other considered cells, except NS10T. Moreover, RHRD12T exhibits the highest write ability due to the use of two extra access transistors and the poor driving ability of the internal nodes. In terms of write delay, RHRD12T shows an improvement of 1.02Â/1.06Â/1.07Â/1.08Â over NS10T/RHD12T/PS10T/RHBD10T at V DD = 1 V. Moreover, RHRD12T is capable of tolerating the highest amount of critical charge among all other comparison cells and is the least susceptible to single-event upsets. All the aforementioned improvements are obtained at the cost of longer read delay.
K E Y W O R D Sdigital circuit, low power design, memory design, read stability, SRAM
| INTRODUCTIONSatellites have become an integral part of human society, as we rely on satellite communication for a wide range of services, from meteorology to disaster monitoring, from navigation systems to military operations, and so on. 1 As the technology is advancing, lightweight satellites are replacing heavyweight satellites because of their higher manufacturing cost. 2 Since lightweight satellites have limited resources, they require high-density memory cells, and static random-access memory (SRAM) cells are the best alternative for space applications because of their high packing density and improved logic performance. 1 Space presents extreme conditions, like temperature fluctuations and radiation. Due to the weak geomagnetic field in space, radiation and energized particles increase. To withstand this harsh environment, special electronic components and circuits are used. Once a radiation particle strikes a logic circuit at its sensitive node, it generates electron-hole pairs (Figure 1A). These pairs become separated and accumulate at the sensitive node. 3 The accumulated charge at the sensitive node then generates a transient voltage pulse. If enough charge (i.e., critical charge, Q C ) is