Reliability Analysis of a Solid Rocket Motor Based on Response Surface Method and Monte Carlo Simulation

41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Volumn , Issue , 2005, Pages

  Bozkaya, Kenan ^a,b   Sümer, Bülent ^a,c   Kuran, Bayindir ^a,d   Ak, Mehmet Ali ^a,d  

^a SCIENTIFIC AND TECHNOLOGICAL RESEARCH COUNCIL OF TURKEY   (Turkey)

^b Systems and Specialty Engineering Division   (Turkey)

^c Propulsion Division   (Turkey)

^d Propulsion and Warhead Technologies Group Coordinator   (Turkey)

Author keywords

[No Author keywords available]

Indexed keywords

BALLISTIC PERFORMANCE; BALLISTIC PROPERTIES; GEOMETRICAL PROPERTY; GEOMETRICAL VARIATIONS; HIGH RELIABILITY; INDIVIDUAL COMPONENTS; MONTE CARLO SIMULATION; MOTOR CASE; NUMERICAL RESULTS; PERFORMANCE FUNCTIONS; PERFORMANCE PARAMETERS; PERFORMANCE REQUIREMENTS; REAL-TIME TESTING; RELIABILITY CALCULATION; RESPONSE SURFACE; RESPONSE SURFACE METHOD; ROCKET MOTOR; SAFETY REQUIREMENTS; SOLID ROCKET MOTORS; STRUCTURAL RELIABILITY; STRUCTURAL SAFETY; UNGUIDED ROCKETS;

BALLISTICS; COMPUTER SIMULATION LANGUAGES; COST BENEFIT ANALYSIS; FAILURE ANALYSIS; MONTE CARLO METHODS; MOTORS; PROPELLANTS; QUALITY ASSURANCE; ROCKET ENGINES; ROCKETS; SAFETY FACTOR; SAFETY TESTING; SPACECRAFT PROPULSION; SURFACE PROPERTIES;

RELIABILITY ANALYSIS;

EID: 84869713379     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (13)

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