Studies on high burning rate composite propellant formulations using TATB as pressure index suppressant

Central European Journal of Energetic Materials

Volumn 9, Issue 3, 2012, Pages 237-249

  Mehilal, ^a   Jawalkar, Shekhar ^a   Kurva, Ramesh ^a   Sundaramoorthy, Nandagopal ^a   Dombe, Ganesh ^a   Singh, Praveen Prakash ^a   Bhattacharya, Bikash ^a  

^a HIGH ENERGY MATERIALS RESEARCH LABORATORY   (India)

Author keywords

Ammonium perchlorate; Composite propellant; Pressure index suppressant; TATB

Indexed keywords

AMMONIUM PERCHLORATES; BURN RATES; BURNING RATE; FRICTION VALUES; HIGH BURNING RATE PROPELLANT; PRESSURE INDEX; PRESSURE RANGES; STANDARD COMPOSITION; TATB; THERMAL AND MECHANICAL PROPERTIES;

MECHANICAL PROPERTIES; VISCOSITY;

COMPOSITE PROPELLANTS;

EID: 84868102978     PISSN: 17337178     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

References (11)

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