000	00000nam 2200000zi 4500
001	9.927847
003	CaOODSP
005	20230928134610
006	m     o  d f
007	cr |n|||||||||
008	230927e198703uuabcad   o    f000 0 eng d
040	|aCaOODSP|beng|erda|cCaOODSP
043	|an-cn-ab
086	1 |aDR52-6/12-1987E-PDF
100	1 |aPenzes, S. G., |eauthor.
245	10|aEnvironmental tests of the ROBOT-X airframe (U) / |cby S.G. Penzes, A.B. Markov, A.E. Turner, and B.G. Boulter.
246	35|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
490	1 |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].
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.
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
710	2 |aDefence Research Establishment Suffield, |eissuing body.
710	1 |aCanada. |bDepartment of National Defence, |eissuing body.
830	#0|aSuffield memorandum ;|vno. 1192.|w(CaOODSP)9.870467
856	40|qPDF|s2.46 MB|uhttps://publications.gc.ca/collections/collection_2023/rddc-drdc/DR52-6-12-1987-eng.pdf
986	|aDRES-M-1192 ;
986	|aSM 1192