Combustion Instability of Solid Propellents - Effect of Oxidizer Particle Size, Oxidizer/Fuel Ratio and Addition of Titanium Dioxide to Plastic Propellents

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Combustion Instability of Solid Propellents - Effect of Oxidizer Particle Size, Oxidizer/Fuel Ratio and Addition of Titanium Dioxide to Plastic Propellents

R. D. Gould

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Title :

Combustion Instability of Solid Propellents - Effect of Oxidizer Particle Size, Oxidizer/Fuel Ratio and Addition of Titanium Dioxide to Plastic Propellents

Contributors:

R. D. Gould (author)

Publication date :

1968

Size :

40 pages

Type of media :

Report

Type of material :

No indication

Language :

English

Keywords :

Rocket Propellants , Combustion stability , Plastic propellants , Propellant additives , Rocket oxidizers , Solid propellants , Acoustic attenuation , Ammonium perchlorates , Burning rate , Particle size distribution , Titanium oxides

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