2018
DOI: 10.22211/cejem/81174
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Optimization of Curing Agents for Linear Difunctional Glycidyl Azide Polymer (GAP), with and without Isocyanate, for Binder Applications

Abstract: Glycidyl Azide Polymer (GAP) is one of the most potential energetic binders for rocket propellants and gas generator compositions. In the present paper GAP of molecular weight (Mn) ~2000 was cured with a mixture of di-and tri-isocyanates without a cross linker. The curing profile and time of curing was recorded using a rheometer. The minimum curing time was observed for samples cured with Desmodour N-100 alone, whereas the maximum curing time was observed for samples cured with a mixture of Desmodour N-100 and… Show more

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Cited by 6 publications
(2 citation statements)
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“…Another approach to curing GAP was adopted by Agawane et al [30], who employed multiple curing agents: mixtures of di-(CI1, CI3) and tri-functional (CI2) isocyanates, an alkyne curing agent (CA6) and, most interestingly, an acrylate-based (CV1) curing agent (Figure 6). Although the authors, similarly to Hagen [28], achieved the best mechanical properties when using a mixture of isocyanate curing agents, they did not attempt sequential curing, which may have resulted in even better properties.…”
Section: Figurementioning
confidence: 99%
“…Another approach to curing GAP was adopted by Agawane et al [30], who employed multiple curing agents: mixtures of di-(CI1, CI3) and tri-functional (CI2) isocyanates, an alkyne curing agent (CA6) and, most interestingly, an acrylate-based (CV1) curing agent (Figure 6). Although the authors, similarly to Hagen [28], achieved the best mechanical properties when using a mixture of isocyanate curing agents, they did not attempt sequential curing, which may have resulted in even better properties.…”
Section: Figurementioning
confidence: 99%
“…Glycidyl azide polymer (GAP) is a binder which is widely used in propellant [1][2][3][4][5][6]. GAP spherical propellant prepared by an internal solution method is one of the most popular components of composite modified double-base (CMDB) propellant [7,8].…”
Section: Introductionmentioning
confidence: 99%