DocumentCode :
2108703
Title :
High performance radiation hardened static random access memory (SRAM) design for space applications
Author :
Doyle, Scott ; Ramaswamy, Srini ; Hoang, Tri ; Rockett, Leonard ; Grembowski, Tim ; Bumgarner, Adam
Author_Institution :
BAE Syst., Manassas, VA, USA
Volume :
4
fYear :
2004
fDate :
6-13 March 2004
Firstpage :
2284
Abstract :
Static random access memory (SRAM) product for advanced space applications must demonstrate high performance to meet the ever increasing data rates of space systems and must be radiation hardened to ensure unfettered, reliable operation in the harsh environments of outer space. High performance and radiation hardness are not mutually exclusive. The challenge confronting present day SRAM development is to concurrently achieve both of these objectives. An SRAM design evaluation methodology is described that uncovers limitations on performance, facilitating the identification of both the limiting mechanisms and the corrective design enhancements. Simulation model to hardware measurement correlation on two designs of radiation tolerant 4 M SRAM product validates the evaluation methodology. The evaluation methodology described herein can be Universally applied to any SRAM design to ensure that the highest performance potential of the design is realized.
Keywords :
CMOS memory circuits; SRAM chips; integrated circuit design; integrated circuit modelling; integrated circuit reliability; performance evaluation; radiation hardening (electronics); space vehicle electronics; SRAM design; SRAM simulation model; data rates; evaluation methodology; hardware correlation; hardware measurement; radiation hardening; space application; static random access memory design; CMOS technology; Design methodology; Hardware; Microelectronics; Power dissipation; Product design; Radiation hardening; Random access memory; SRAM chips; Space technology;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace Conference, 2004. Proceedings. 2004 IEEE
ISSN :
1095-323X
Print_ISBN :
0-7803-8155-6
Type :
conf
DOI :
10.1109/AERO.2004.1368022
Filename :
1368022
Link To Document :
بازگشت