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| 02023nam 2200385zi 4500 |
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001 | 9.893606 |
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003 | CaOODSP |
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005 | 20221107173508 |
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006 | m o d f |
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007 | cr bn||||||||| |
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008 | 201116e197207##oncad ob f000 0 eng d |
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040 | |aCaOODSP|beng|erda|cCaOODSP |
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043 | |an-cn--- |
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086 | 1 |aCo24-3/7-1232-1972E-PDF |
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100 | 1 |aHarrison, T. D., |eauthor. |
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245 | 10|aAtmospheric drag distortion of long spinning flexible antennas / |cby T.D. Harrison, F.R. Vigneron. |
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264 | 1|aOttawa : |bCommunications Research Centre, Department of Communications, |cJuly 1972. |
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300 | |a1 online resource (iii, 10 pages) : |billustration, graphs. |
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336 | |atext|btxt|2rdacontent |
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337 | |acomputer|bc|2rdamedia |
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338 | |aonline resource|bcr|2rdacarrier |
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490 | 1 |aCRC report ; |vno. 1232 |
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500 | |aDigitized edition from print [produced by Innovation, Science and Economic Development Canada]. |
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504 | |aIncludes bibliographical references (page 6). |
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520 | 3 |a"This report presents a mathematical model of the distortion due to atmospheric drag on spinning flexible antennas. Using parameters compatible with those of a satellite at one time proposed for the ISIS series, this model is solved for the different modes of deflection. It is concluded that the minimum perigee height should be not less than 500 km and the minimum spin rate be not less than 0.1 rpm"--Abstract, page 1. |
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650 | 0|aDrag (Aerodynamics)|xMathematical models. |
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650 | 0|aAntennas (Electronics) |
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650 | 0|aArtificial satellites|xAerodynamics. |
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650 | 6|aTraînée (Aérodynamique)|xModèles mathématiques. |
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650 | 6|aAntennes (Électronique) |
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650 | 6|aSatellites artificiels|xAérodynamique. |
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710 | 2 |aCommunications Research Centre (Canada), |eissuing body. |
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830 | #0|aCRC report ;|vno. 1232.|w(CaOODSP)9.882492 |
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856 | 40|qPDF|s1.15 MB|uhttps://publications.gc.ca/collections/collection_2020/isde-ised/Co24/Co24-3-7-1232-1972-eng.pdf |
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