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| 02247nam 2200445zi 4500 |
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001 | 9.927847 |
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003 | CaOODSP |
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005 | 20230928134610 |
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006 | m o d f |
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007 | cr |n||||||||| |
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008 | 230927e198703uuabcad o f000 0 eng d |
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040 | |aCaOODSP|beng|erda|cCaOODSP |
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043 | |an-cn-ab |
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086 | 1 |aDR52-6/12-1987E-PDF |
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100 | 1 |aPenzes, S. G., |eauthor. |
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245 | 10|aEnvironmental tests of the ROBOT-X airframe (U) / |cby S.G. Penzes, A.B. Markov, A.E. Turner, and B.G. Boulter. |
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246 | 35|aEnvironmental tests of the ROBOT-X airframe |
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264 | 1|aRalston, Alberta : |bDefence Research Establishment Suffield, |cMarch 1987. |
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300 | |a1 online resource (vi, 15 pages, [36] pages in various pagings) : |billustrations, charts |
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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 |aSuffield memorandum ; |vno. 1192 |
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500 | |a"Project No. 031SE"--title page. |
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500 | |aB.G. Boulter affiliated with Boeing of Canada Ltd., Winnipeg, Manitoba. |
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500 | |aDigitized edition from print [produced by Defence Research and Development Canada]. |
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520 | 3 |a"Environmental tests are described in which the ROBOT-X airframe was subjected to a wide range of ambient temperatures, from a minimum of -50C to a maximum of +58C. No unexpected problems were encountered. Valuable insight was gained into airframe thermal response under extreme ambient temperature conditions"--abstract. |
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650 | 0|aCruise missiles|zCanada|xTesting. |
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650 | 0|aAluminum|xEffect of temperature on. |
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650 | 0|aPolymers|xEffect of temperature on. |
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650 | 6|aMissiles de croisière|zCanada|xTests. |
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650 | 6|aAluminium|xEffets de la température sur. |
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650 | 6|aPolymères|xEffets de la température sur. |
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655 | 7|aTechnical reports|2lcgft |
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655 | 7|aRapports techniques|2rvmgf |
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710 | 2 |aDefence Research Establishment Suffield, |eissuing body. |
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710 | 1 |aCanada. |bDepartment of National Defence, |eissuing body. |
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830 | #0|aSuffield memorandum ;|vno. 1192.|w(CaOODSP)9.870467 |
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856 | 40|qPDF|s2.46 MB|uhttps://publications.gc.ca/collections/collection_2023/rddc-drdc/DR52-6-12-1987-eng.pdf |
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