SEE IN-FLIGHT MEASUREMENT AN THE MIR ORBITAL STATION

Authors
FALGUERE D DUZELLIER S ECOFFET R
Citation
D. Falguere et al., SEE IN-FLIGHT MEASUREMENT AN THE MIR ORBITAL STATION, IEEE transactions on nuclear science, 41(6), 1994, pp. 2346-2352
Citations number
6
Categorie Soggetti
Nuclear Sciences & Tecnology","Engineering, Eletrical & Electronic
Journal title
IEEE transactions on nuclear science → ACNP
ISSN journal
00189499
Volume
41
Issue
6
Year of publication
1994
Part
1
Pages
2346 - 2352
Database
ISI
SICI code
0018-9499(1994)41:6<2346:SIMATM>2.0.ZU;2-4
Abstract
SEE spaceflight measurements are presented on HM65756 SRAM from Matra- MHS, Seeq 28C256 and Motorola MC68020 microprocessor (bulk version) in the MIR station orbit (350 km altitude, 51.6 degrees inclination). Ac celerator testing (heavy ion and proton) of flight spares permits the prediction of the event rates using standard model such as CREME and S PACERAD(1) as well as characterisations of the flight components allow ing the comparison of in-orbit observations. Event rate prediction and ground-testing data are compared.