SYSTEM HARDENING APPROACHES FOR A LEO SATELLITE WITH RADIATION TOLERANT PARTS

Authors
LUM GK BENNETT NR LOCKHART JM
Citation
Gk. Lum et al., SYSTEM HARDENING APPROACHES FOR A LEO SATELLITE WITH RADIATION TOLERANT PARTS, IEEE transactions on nuclear science, 44(6), 1997, pp. 2026-2033
Citations number
9
Categorie Soggetti
Nuclear Sciences & Tecnology","Engineering, Eletrical & Electronic
Journal title
IEEE transactions on nuclear science → ACNP
ISSN journal
00189499
Volume
44
Issue
6
Year of publication
1997
Part
1
Pages
2026 - 2033
Database
ISI
SICI code
0018-9499(1997)44:6<2026:SHAFAL>2.0.ZU;2-N
Abstract
With the combination of various space environmental models and hardeni ng approaches one can design a LEO spacecraft with affordable nonharde ned parts technologies. Hardening approaches for the Gravity Probe-B s atellite will be discussed.