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040 |aCaOODSP|beng|erda|cCaOODSP
043 |an-cn---
0861 |aCo24-3/1-82-023E-PDF
1001 |aSincarsin, G. B., |eauthor.
24510|aComputer code for MSAT structural dynamics model (preliminary) / |cG.B. Sincarsin, I.A. Stoddard, P.C. Hughes.
264 1|aOttawa : |bDepartment of Communications, |cMarch 1982.
300 |a1 online resource (1 volume (various pagings)) : |billustrations.
336 |atext|btxt|2rdacontent
337 |acomputer|bc|2rdamedia
338 |aonline resource|bcr|2rdacarrier
4901 |aDOC contractor report ; |vDOC-CR-SP-82-023
500 |aDigitized copy from print [produced by Innovation, Science and Economic Development Canada].
500 |a"Dynacon Report MSAT-5."
500 |a"This report was prepared for Spar Aerospace Ltd. under Subcontract No. 11138TC"--Foreword.
504 |aIncludes bibliographical references (page 23).
520 |a"It is assumed that MSAT consists of four substructures (Figs. 1.1 and 1.2): a main bus, a solar array, a tower, and a large parabolic dish reflector. The latter three are allowed to be structurally flexible, and their substructure models are presumed to be specified either in terms of mass and stiffness matrices, or modal data (frequencies and modal vectors). This report shows how to combine these general substructural models into an overall structural model for the spacecraft"--Summary, page iv.
650 0|aArtificial satellites|xDynamics.
650 0|aArtificial satellites|xControl systems|xComputer programs.
650 6|aSatellites artificiels|xDynamique.
650 6|aSatellites artificiels|xSystèmes de commande|xLogiciels.
7101 |aCanada. |bDepartment of Communications, |eissuing body.
7102 |aDynacon Enterprises Ltd., |econsultant.
7102 |aSpar Aerospace Ltd., |econsultant.
830#0|aDOC contractor report (Canada. Department of Communications)|vDOC-CR-SP-82-023.|w(CaOODSP)9.869864
85640|qPDF|s1.07 MB|uhttps://publications.gc.ca/collections/collection_2025/isde-ised/co24/Co24-3-1-82-023-eng.pdf