High strain-rate impact studies of predamaged rocket propellants. I. Characterization of damage using a cumulative damage failure criterion

Combustion and Flame

Volumn 104, Issue 4, 1996, Pages 524-534

  Ho, S Y ^a  

^a AERO AND MAR RESEARCH LABORATORY   (Australia)

Author keywords

[No Author keywords available]

Indexed keywords

MODELS; ROCKETS;

AMMONIUM NITRATES; BUTADIENE DERIVATIVE POLYMER; EXPERIMENTAL STUDY; STRENGTH; STRESS CRACKING;

SOLID PROPELLANTS;

PROPELLANT;

ARTICLE; COMBUSTION; EXPLOSION; MATHEMATICAL ANALYSIS; MECHANICS; MODEL; PRIORITY JOURNAL; TENSION; VISCOELASTICITY;

EID: 0029981191     PISSN: 00102180     EISSN: None     Source Type: Journal    
DOI: 10.1016/0010-2180(95)00166-2     Document Type: Article

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