Kinetic of Deep High-Temperature Decomposition of Model and Commercial AP-Based Composite Solid Propellants

2008 ◽  
pp. 137-156
Author(s):  
Alexander S. Shteinberg
Keyword(s):  
High Temperature ◽  
Solid Propellants ◽  
Temperature Decomposition ◽  
Composite Solid Propellants ◽  
Composite Solid

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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