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New Propellant Component, Part I. Study of 4,6‐Dinitroamino‐1,3,5‐Triazine‐2(1 H)‐One (DNAM)
Author(s) -
Simões P.,
Pedroso L.,
Portugal A.,
Carvalheira P.,
Campos J.
Publication year - 2001
Publication title -
propellants, explosives, pyrotechnics
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.56
H-Index - 65
eISSN - 1521-4087
pISSN - 0721-3115
DOI - 10.1002/1521-4087(200112)26:6<273::aid-prep273>3.0.co;2-0
Subject(s) - propellant , dnam , sensitivity (control systems) , stability (learning theory) , computer science , materials science , chemistry , aerospace engineering , engineering , biochemistry , gene expression , dna methylation , gene , electronic engineering , machine learning
This paper reports a study of the synthesis and characterization of 4,6‐dinitroamino‐1,3,5‐triazine‐2(1 H)‐one (DNAM) carried out under the perspective of looking for new ingredients in propellant formulations. Emphasis is given to the characterization of DNAM. The following attributes were identified: low sensitivity to impact and friction, thermal stability over a wide temperature range, energetic nature, high density, and interesting particle size distribution. In Part 2 a preliminary evaluation of DNAM capabilities in a propellant formulation will be presented.