Review of Composite Propellant Burn Rate Modeling

AIAA Journal ◽  
1980 ◽  
Vol 18 (3) ◽  
pp. 277-293 ◽  
Author(s):  
Norman S. Cohen
Keyword(s):  
Composite Propellant ◽  
Burn Rate

Graphene-iron oxide nanocomposite (GINC): an efficient catalyst for ammonium perchlorate (AP) decomposition and burn rate enhancer for AP based composite propellant

RSC Advances ◽  
2015 ◽  
Vol 5 (3) ◽  
pp. 1950-1960 ◽  
Author(s):  
Abhijit Dey ◽  
Javaid Athar ◽  
Pankaj Varma ◽  
Hima Prasant ◽  
Arun K. Sikder ◽  
...  
Keyword(s):  
Iron Oxide ◽  
Ammonium Perchlorate ◽  
Composite Propellant ◽  
Efficient Catalyst ◽  
Burn Rate

Development of a facile and ecofriendly route for the synthesis of GINC, followed by characterization and evaluation in propellants for missiles.

DEVELOPMENT OF A BALLISTIC EVALUATION MOTOR FOR KNSU BURN RATE MEASUREMENTS

2020 ◽  
Author(s):  
Carlos Américo ◽  
Diego Fernando Moro ◽  
Carlos Henrique Marchi ◽  
Filipe Aguiar
Keyword(s):  
Burn Rate
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