burn rate modifier
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Author(s):  
Krzysztof Motyl ◽  
Bogdan Zygmunt ◽  
Andrzej Cholewiak ◽  
Mirosław Szczepanik

Nitrocellulose and nitroglycerin are the main components of double-base propellants comprising up to 95% of their total mass. A chemical stabiliser and a burn rate modifier are required components, added in amounts of several percent. The study analyses the effect of carbon black content, contributing less than 1% of the propellant mass, on the burning rate of differently shaped propelling charges. The experiments, carried out on high energetic, double-base propelling charges, showed that the carbon black content significantly affects the burning rate of the propelling charge in the rocket motor chamber.


2016 ◽  
Vol 12 (4) ◽  
pp. 297-304 ◽  
Author(s):  
D. Chaitanya Kumar Rao ◽  
Narendra Yadav ◽  
Puran Chandra Joshi

2011 ◽  
Vol 123 (20) ◽  
pp. 4720-4722 ◽  
Author(s):  
Jesse J. Sabatini ◽  
Jay C. Poret ◽  
Russell N. Broad

2011 ◽  
Vol 50 (20) ◽  
pp. 4624-4626 ◽  
Author(s):  
Jesse J. Sabatini ◽  
Jay C. Poret ◽  
Russell N. Broad

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