Deflection of multicellular inflatable tubes for redundant space structures

Journal of Spacecraft and Rockets

Volumn 39, Issue 5, 2002, Pages 695-700

  Sakamoto, Hiraku ^a,c,d   Natori, M C ^a,e   Miyazaki, Yasuyuki ^b,f  

^a JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

^b NIHON UNIVERSITY   (Japan)

^c UNIVERSITY OF TOKYO   (Japan)

^d University of Colorado at Boulder   (United States)

^e Space Structures Laboratory ^*  (Japan)

^f Department of Aerospace Engineering   (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; DEFLECTION (STRUCTURES); FINITE ELEMENT METHOD; HARDENING; INFLATABLE STRUCTURES; MATHEMATICAL MODELS; PRESSURIZATION; RIGIDITY; STIFFNESS; STRENGTH OF MATERIALS; STRUCTURAL ANALYSIS; TUBES (COMPONENTS);

BALLOON SATELLITES; EULER-BERNOULLI BEAM THEORY; MULTICELLULAR CANTILEVER INFLATABLE TUBES; REDUNDANT SPACE STRUCTURES; RIGIDIZATION; SLACKENING EFFECT;

SATELLITES;

EID: 0036757404     PISSN: 00224650     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.3892     Document Type: Article

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