Determination of Primary Amine Content in Bonding Agent Used in Composite Solid Propellants

2014 ◽  
Vol 39 (4) ◽  
pp. 538-544 ◽  
Author(s):  
José I. S. Oliveira ◽  
Darci C. Pires ◽  
Milton F. Diniz ◽  
Jorge L. Siqueira ◽  
Elizabeth C. Mattos ◽  
...  
Keyword(s):  
Primary Amine ◽  
Bonding Agent ◽  
Solid Propellants ◽  
Amine Content ◽  
Composite Solid Propellants ◽  
Composite Solid

scholarly journals Effect of bonding agent production materials on the mechanical properties of composite solid rocket propellant

2018 ◽  
Vol 189 ◽  
pp. 08001 ◽  
Author(s):  
Ali.M.Abd elall ◽  
Guo Lin
Keyword(s):  
Mechanical Properties ◽  
Solid Particles ◽  
Bonding Agent ◽  
Solid Propellants ◽  
Solid Rocket Propellant ◽  
Bonding Agents ◽  
Composite Solid Propellants ◽  
Good Strain ◽  
Solid Rocket ◽  
Composite Solid

An effective pathway was explored to design and select proper bonding agents that could effectively improve the interfacial interactions between bonding agents and solid particles, modern types of composite solid propellants focused on increasing the mechanical properties in order to withstand stresses produced due to various loading conditions, changes in environmental condition, transportation and handling. In this work, the study show that the effect of solvent in production of bonding agent has a different impact on the mechanical properties as the polar solvent in formulation S3 has a good strain values corresponding to the stress. Also the changing of the percentage of CuCl2 has a significant effect on mechanical properties as giving high value of strain with the percentage of 4.5 % and returns back the value of strain decrease with increase the percentage of CuCl2 to give the lowest values of the strain corresponding to the stress value with percentage 7.5 %.

scholarly journals Cu–Co–O nano-catalysts as a burn rate modifier for composite solid propellants

2016 ◽  
Vol 12 (4) ◽  
pp. 297-304 ◽  
Author(s):  
D. Chaitanya Kumar Rao ◽  
Narendra Yadav ◽  
Puran Chandra Joshi
Keyword(s):  
Solid Propellants ◽  
Composite Solid Propellants ◽  
Burn Rate Modifier ◽  
Nano Catalysts ◽  
Burn Rate ◽  
Composite Solid

scholarly journals DETONATION NANODIAMOND AS PROSPECTIVE COMPONENT OF COMPOSITE SOLID PROPELLANTS

2018 ◽  
Vol 59 (8) ◽  
pp. 96
Author(s):  
Valentin A. Gorbachev ◽  
Evgeniy Yu. Ubey - Volk ◽  
Nikolay V. Shevchenko ◽  
Alexandr A. Golubev
Keyword(s):  
Fuel Composition ◽  
Solid Propellants ◽  
Detonation Nanodiamond ◽  
Metal Free ◽  
Composite Solid Propellants ◽  
Composite Solid

In this articlethe the possibility of application of detonation nanodiamond (DND) as a prospective component of composite solid propellants (CSP) and additive approach to optimization of fuel compositions based on binary fuel compositions is considered. The introduction to the fuel composition of DND allows creating a metal-free CSP with increased energy-to-mass characteristics. Usage of the additive approach for calculations when creating new prospective compositions of CSP allows reducing significantly the volume of work to optimize the fuel compositions and to simplify the process of thermodynamic engineering.

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