Damage detection in satellite bolted joints

Proceedings of the ASME Conference on Smart Materials, Adaptive Structures and Intelligent Systems, SMASIS2008

Volumn 2, Issue , 2008, Pages 209-218

  Doyle, Derek ^a   Zagrai, Andrei ^b   Arritt, Brandon ^a   Cakan, Hakan ^b  

^a AIR FORCE RESEARCH LABORATORY   (United States)

^b NEW MEXICO INSTITUTE OF MINING AND TECHNOLOGY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE STRUCTURE; COMPLEX STRUCTURE; CRITICAL SYSTEMS; CURRENT LIMITATION; ELASTIC BEHAVIOR; EXPERIMENTAL DATA; FLIGHT QUALIFICATION; LAUNCH VEHICLE; LOCALIZATION POTENTIAL; MECHANICAL IMPEDANCES; NON-LINEAR RESPONSE; OPERATIONALLY RESPONSIVE SPACES; PIEZOELECTRIC WAFER ACTIVE SENSORS; REAL-TIME ASSESSMENT; SATELLITE OPERATIONS; SATELLITE STRUCTURE; THIN PLATE; TIME SPENT;

BOLTED JOINTS; DAMAGE DETECTION; INTELLIGENT MATERIALS; INTELLIGENT SYSTEMS; LAUNCH VEHICLES; LAUNCHING; SATELLITES; SENSORS; STRUCTURAL HEALTH MONITORING;

BOLTS;

EID: 78149384164     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/SMASIS2008-550     Document Type: Conference Paper

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