X2000 power system electronics development

Author

Carr, Gregory A. ; Wester, Gene ; Danielak, Bob ; Sauers, James D. ; Hogue, David ; Holic, John

Author_Institution

Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA

Volume

5

fYear

2000

fDate

2000

Firstpage

341

Abstract

The Deep Space System Technology Program (X2000) is designed to provide advanced flight and ground systems for the exploration of the outer planets. The X2000 Integrated First Delivery Project under DSST will provide flight avionics for the first set of mission customers, Europa Orbiter, Pluto/Kuiper Express and Solar Probe. These missions provide a challenge in terms of extreme environmental requirements. The key driving requirements are the one mega-rad total ionizing dose and the fifteen-year life. The X2000 power system electronics must reduce its power, mass and volume envelope by incorporating new technology developed by industry partners. The combination of MCM packaging, rad-hard mixed signal ASICs and next-generation-power devices increases the packaging density of the power system electronics

Keywords

integrated circuit packaging; mixed analogue-digital integrated circuits; multichip modules; power integrated circuits; power semiconductor switches; space vehicle electronics; space vehicle power plants; Deep Space System Technology Program; Europa Orbiter; Integrated First Delivery Project; MCM packaging; Pluto/Kuiper Express; Solar Probe; X2000 program; advanced flight and ground systems; extreme environmental requirements; flight avionics; high total ionizing dose; next-generation-power devices; packaging density; power system electronics development; radiation-hard mixed signal ASIC; Aerospace electronics; Decision support systems; Electronics industry; Electronics packaging; Industrial electronics; Planets; Pluto; Power systems; Probes; Space technology;

fLanguage

English

Publisher

ieee

Conference_Titel

Aerospace Conference Proceedings, 2000 IEEE

Conference_Location

Big Sky, MT

ISSN

1095-323X

Print_ISBN

0-7803-5846-5

Type

conf

DOI

10.1109/AERO.2000.878507

Filename

878507