Theoretical prediction of erosive burning characteristics of solid rocket propellant based on burning rate dependence of pressure and initial temperature and its energetic characteristics

1976 ◽  
Author(s):  
B. JOJIC ◽  
D. BLAGOJEVIC
Keyword(s):  
Theoretical Prediction ◽  
Burning Rate ◽  
Initial Temperature ◽  
Rate Dependence ◽  
Solid Rocket Propellant ◽  
Rocket Propellant ◽  
Erosive Burning ◽  
Solid Rocket

Measurement system for determining solid rocket propellant burning rate using transmission microwave interferometry

1997 ◽  
Author(s):  
Vladica Bozic ◽  
Djordje Blagojevic ◽  
Bozidar Anicin ◽  
Vladica Bozic ◽  
Djordje Blagojevic ◽  
...  
Keyword(s):  
Burning Rate ◽  
Measurement System ◽  
Solid Rocket Propellant ◽  
Rocket Propellant ◽  
Microwave Interferometry ◽  
Solid Rocket

Analysis of aluminum particle combustion in a downward burning solid rocket propellant

Fuel ◽  
2019 ◽  
Vol 237 ◽  
pp. 405-412 ◽  
Author(s):  
Castillo Griego ◽  
Nadir Yilmaz ◽  
Alpaslan Atmanli
Keyword(s):  
Aluminum Particle ◽  
Solid Rocket Propellant ◽  
Rocket Propellant ◽  
Particle Combustion ◽  
Solid Rocket
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