000	02351cam  2200433zi 4500
001	9.888756
003	CaOODSP
005	20221107172101
006	m     o  d f
007	cr |n|||||||||
008	200629e19820518onca    o    f000 0 eng d
040	|aCaOODSP|beng|erda|cCaOODSP
086	1 |aCo24-3/1-82-048E-PDF
100	1 |aGomi, T., |eauthor.
245	12|aA study and specification of a distributed fault-tolerant microprocessor system : |ban executive summary / |cauthors: T. Gomi, M. Inwood ; prepared by: Eidetic Systems Corporation.
264	1|aOttawa, Canada : |bDepartment of Communications, Space Program, |cMay 18, 1982.
300	|a1 online resource (22 pages) : |billustrations.
336	|atext|btxt|2rdacontent
337	|acomputer|bc|2rdamedia
338	|aonline resource|bcr|2rdacarrier
490	1 |aDOC contractor report ; |vDOC-CR-SP-82-048
500	|a"Unclassified."
500	|a"SN: OER81-03138."
500	|a"Department of Supply and Services Contract no: 3ER.36100-1-0274."
500	|aDigitized copy from print [produced by Innovation, Science and Economic Development Canada].
520	|a"The early application of fault-tolerance to spacecraft was an expensive procedure. The burden it involved was only justified in deep-space missions where long-term survival was essential to the success of the project. Typically, systems were designed using well-proven technology which, by launch date, was becoming outmoded because of the lengthy development time. Thus each mission required a fresh start, with inevitable high development costs"--Introduction, page 1.
650	0|aAirborne computers.
650	0|aFault-tolerant computing.
650	0|aMicroprocessors.
650	0|aSpace vehicles.
650	6|aOrdinateurs de bord (Instruments d'aéronautique)
650	6|aTolérance aux fautes (Informatique)
650	6|aMicroprocesseurs.
650	6|aVéhicules spatiaux.
710	1 |aCanada. |bDepartment of Communications. |bSpace Program, |eissuing body.
710	2 |aEidetic Systems Corporation, |econsultant.
830	#0|aDOC contractor report (Canada. Department of Communications)|vDOC-CR-SP-82-048.|w(CaOODSP)9.869864
856	40|qPDF|s2.86 MB|uhttps://publications.gc.ca/collections/collection_2020/isde-ised/Co24/Co24-3-1-82-048-eng.pdf