Kumar, Deepak; Singh, Hema; Maurya, Mehilal; Nguyen, Van-Huy; Vo, Dai-Viet N.; Sharma, Ajit; Banerjee, Shaibal published the artcile< Novel evaluation enhancement role of poly (1-(3-nitrophenyl)-1H-1,2,3-triazol-4-yl) acrylate materials for propellant composite formulation>, Computed Properties of 112-63-0, the main research area is propellant composite nitrophenyl triazolyl acrylate enhancement.
The performance of solid propellants is often tailored by incorporating energetic materials such as novel oxidizers, energetic binders, and ballistic modifiers. Metal oxide nanoparticles are known for their persuasive nature to modify burning rate of ammonium perchlorate based composite propellants. In the present work, nano iron oxide and poly (1-(3-nitrophenyl)-1H-1,2,3-triazol-4-yl) acrylate are incorporated in the composite propellant formulation by partly replacing coarse ammonium perchlorate (AP) as well as hydroxy terminated polybutadiene (HTPB), resp., and different properties were evaluated. The mech. properties data revealed that on increasing the percentage of polymer in the composition by partly replacing HTPB, there is an increase in tensile strength while decreasing elongation percentage. The data of ballistic properties revealed that on incorporation of nano iron oxide in the composition enhances the burning rate while on partial replacement of HTPB with polymer there is a decrease in burning rate from 11.95 mm s-1 to 8.75 mm s-1, resp. was observed
Materials Letters published new progress about Combustion. 112-63-0 belongs to class esters-buliding-blocks, and the molecular formula is C19H34O2, Computed Properties of 112-63-0.
Referemce:
Ester – Wikipedia,
Ester – an overview | ScienceDirect Topics