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008250423t19951995qucd    ob   f000 0 eng d
040 |aCaOODSP|beng|erda|cCaOODSP
0410 |aeng|beng|bfre
0861 |aD68-23/4-1995E-PDF
1001 |aAhad, E., |eauthor.
24510|aImproved process for the synthesis of second generation branched gap / |cby E. Ahad.
264 1|aValcartier, Québec : |bDefence Research Establishment = Centre de recherches pour la défense : |bDepartment of National Defence Canada, Research and Development Branch = Ministère de la Défense nationale, Bureau - recherche et développement, |c1995.
264 4|c©1995
300 |a1 online resource (viii, 33 pages, 21 unnumbered pages) : |bgraphs.
336 |atext|btxt|2rdacontent
337 |acomputer|bc|2rdamedia
338 |aonline resource|bcr|2rdacarrier
4901 |aDREV - R ; |v9414
500 |a"April/avril 1995."
500 |aDigitized edition from print [produced by Defence Research and Development Canada].
504 |aIncludes bibliographical references (pages 30-33).
520 |a"Glycidyl Azide Polymer (GAP) is a potential energetic binder for rocket propellants with reduced smoke and low vulnerability as well as for insensitive composite explosives and gun propellants. For these reasons, GAP is considered as an attractive substitute for the inert hydroxy-terminated polybutadiene conventional binder currently used in energetic formulations such as the CRV-7 rocket motor"--Executive summary, page v.
546 |aIncludes abstracts in English and French.
650 0|aPolymerization.
650 0|aPolyols.
650 6|aPolymérisation.
650 6|aPolyalcools.
7102 |aDefence Research Establishment Valcartier, |eissuing body.
7101 |aCanada. |bDepartment of National Defence. |bResearch and Development Branch, |eissuing body.
830#0|aDREV - R (1995)|v9414.|w(CaOODSP)9.943555
85640|qPDF|s2.44 MB|uhttps://publications.gc.ca/collections/collection_2025/rddc-drdc/D68-23-4-1995-eng.pdf