000	02254cam  2200385zi 4500
001	9.892798
003	CaOODSP
005	20221107173253
006	m     o  d f
007	cr bn|||||||||
008	201023s1969    onca    ob   f000 0 eng d
040	|aCaOODSP|beng|erda|cCaOODSP
086	1 |aCo24-3/7-1206-1969E-PDF
100	1 |aVigneron, F. R., |eauthor.
245	10|aElastic stability and equilibrium configuration of earth pointing satellites with long appendages / |cby F.R. Vigneron and T. Garrett.
264	1|aOttawa : |bCommunications Research Centre, |c1969.
300	|a1 online resource (iii, 22 pages) : |billustrations.
336	|atext|btxt|2rdacontent
337	|acomputer|bc|2rdamedia
338	|aonline resource|bcr|2rdacarrier
490	1 |aCRC report ; |vno. 1206
500	|a"National Space Telecommunications Laboratory."
500	|a"Published November 1969."
500	|aDigitized edition from print [produced by Innovation, Science and Economic Development Canada].
504	|aIncludes bibliographical references (page 19).
520	3 |a"The elastic stability of the booms on a gravity gradient stabilized Alouette type satellite is investigated to determine the critical lengths above which the booms will take on large deflect ions under the influence of the gravitational and centrifugal force fields. If the booms are not structurally damaged by the large deflections, the satellite may take up one of several stable configurations. A criterion involving the boom lengths is derived for the stability of the gravity gradient orientation for zero boom deflections. The derivation includes the flexibility of the booms"--Abstract, page 1.
530	|aIssued also in print format.
650	0|aArtificial satellites|xStability.
650	0|aArtificial satellites|xAttitude control systems.
650	6|aSatellites artificiels|xStabilité.
650	6|aSatellites artificiels|xSystèmes de commande d'orientation.
710	2 |aCommunications Research Centre (Canada), |eissuing body.
830	#0|aCRC report ;|vno. 1206.|w(CaOODSP)9.882492
856	40|qPDF|s956 KB|uhttps://publications.gc.ca/collections/collection_2020/isde-ised/Co24/Co24-3-7-1206-1969-eng.pdf