DocumentCode
2290543
Title
Application of test effectiveness in spacecraft testing
Author
Lang, Paul ; Card, Michael ; Saalwaechter, Susie ; Godkin, Todd
Author_Institution
SRS Technol., Arlington, VA, USA
fYear
1995
fDate
16-19 Jan 1995
Firstpage
486
Lastpage
495
Abstract
This article summarizes test design practices of selected NASA Centers and prime contractors as they are used to evaluate the performance and reliability of space mission payloads. It also reports the use of previous relevant test experience to avoid risk in the design of future spacecraft and enhance test programs. Test effectiveness (TE) is defined as the ability of a test to accurately emulate the expected mission environment, and reliably detect failure causing defects before launch. These twin objectives determine the value of a test program relative to project funding
Keywords
aerospace testing; design engineering; failure analysis; reliability; space vehicles; NASA; contractors; design; failure; mission environment; performance; reliability; space mission payloads; spacecraft testing; test design practices; test effectiveness; Aerospace engineering; Aerospace testing; Isolation technology; NASA; Payloads; Qualifications; Reliability engineering; Space technology; Space vehicles; System testing;
fLanguage
English
Publisher
ieee
Conference_Titel
Reliability and Maintainability Symposium, 1995. Proceedings., Annual
Conference_Location
Washington, DC
ISSN
0149-144X
Print_ISBN
0-7803-2470-6
Type
conf
DOI
10.1109/RAMS.1995.513289
Filename
513289
Link To Document