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Volumn 4, Issue , 2003, Pages 3095-3103

A study of a prototype actuator concept for membrane boundary control

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; BOUNDARY CONDITIONS; INFLATABLE EQUIPMENT; MEMBRANES; PIEZOELECTRIC DEVICES; THIN FILMS; VIBRATION CONTROL;

EID: 0042510991     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (18)

References (5)
  • 1
    • 0010452694 scopus 로고    scopus 로고
    • Gossamer spacecraft: Membrane and inflatable structures technology for space applications
    • Jenkins, C.H.M; "Gossamer Spacecraft: Membrane and Inflatable Structures Technology for Space Applications," AIAA, Progress in Astronautics and Aeronautics Volume 191, 2001.
    • (2001) AIAA, Progress in Astronautics and Aeronautics , vol.191
    • Jenkins, C.H.M.1
  • 4
    • 24244459399 scopus 로고    scopus 로고
    • Thin-skin deployable mirrors for remote sensing systems
    • Sandia Report SAND2001-0101 January
    • Henson, T.D., Wehlburg, J.C., Redmond, J.M., Main, J. A. and Martin, J.W.; "Thin-Skin Deployable Mirrors for Remote Sensing Systems," Sandia Report SAND2001-0101 January 2001.
    • (2001)
    • Henson, T.D.1    Wehlburg, J.C.2    Redmond, J.M.3    Main, J.A.4    Martin, J.W.5


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.