Integrated vibration control for the apparatus cabin of CZ-3A launch vehicle

Journal of Spacecraft and Rockets

Volumn 38, Issue 3, 2001, Pages 374-379

  Zhang, J H ^a,c   Xie, S L ^a,d   Zhang, X N ^a,c   Li, Z M ^b,e  

^a XI'AN JIAOTONG UNIVERSITY   (China)

^b CHINA ACADEMY OF LAUNCH VEHICLE TECHNOLOGY   (China)

^c Department of Engineering Mechanics ^*  (China)

^d Theory of Lubrication and Bearing Institute   (China)

^e Air Force   (China)

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; DAMPING; HONEYCOMB STRUCTURES; LAUNCHING; NATURAL FREQUENCIES; PIEZOELECTRIC DEVICES; VIBRATION CONTROL; VIBRATIONS (MECHANICAL); VISCOELASTICITY;

LAUNCH VEHICLES;

SPACECRAFT;

EID: 0035330731     PISSN: 00224650     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.3711     Document Type: Article

References (13)

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12. A new active constrained layer configuration with enhanced boundary actions