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008230927e198703uuabcad   o    f000 0 eng d
040 |aCaOODSP|beng|erda|cCaOODSP
043 |an-cn-ab
0861 |aDR52-6/12-1987E-PDF
1001 |aPenzes, S. G., |eauthor.
24510|aEnvironmental tests of the ROBOT-X airframe (U) / |cby S.G. Penzes, A.B. Markov, A.E. Turner, and B.G. Boulter.
24635|aEnvironmental tests of the ROBOT-X airframe
264 1|aRalston, Alberta : |bDefence Research Establishment Suffield, |cMarch 1987.
300 |a1 online resource (vi, 15 pages, [36] pages in various pagings) : |billustrations, charts
336 |atext|btxt|2rdacontent
337 |acomputer|bc|2rdamedia
338 |aonline resource|bcr|2rdacarrier
4901 |aSuffield memorandum ; |vno. 1192
500 |a"Project No. 031SE"--title page.
500 |aB.G. Boulter affiliated with Boeing of Canada Ltd., Winnipeg, Manitoba.
500 |aDigitized edition from print [produced by Defence Research and Development Canada].
5203 |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.
650 0|aCruise missiles|zCanada|xTesting.
650 0|aAluminum|xEffect of temperature on.
650 0|aPolymers|xEffect of temperature on.
650 6|aMissiles de croisière|zCanada|xTests.
650 6|aAluminium|xEffets de la température sur.
650 6|aPolymères|xEffets de la température sur.
655 7|aTechnical reports|2lcgft
655 7|aRapports techniques|2rvmgf
7102 |aDefence Research Establishment Suffield, |eissuing body.
7101 |aCanada. |bDepartment of National Defence, |eissuing body.
830#0|aSuffield memorandum ;|vno. 1192.|w(CaOODSP)9.870467
85640|qPDF|s2.46 MB|uhttps://publications.gc.ca/collections/collection_2023/rddc-drdc/DR52-6-12-1987-eng.pdf