Design and fabrication of CFRP interstage attach fitting for launch vehicles

Journal of Aerospace Engineering

Volumn 12, Issue 3, 1999, Pages 83-91

  Hou, An ^a,b   Gramoll, Kurt ^c  

^a Sci Delta Airlines   (United States)

^b Georgia Institute of Technology   (United States)

^c University of Oklahoma   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BUCKLING; CARBON FIBER REINFORCED PLASTICS; COMPRESSIVE STRENGTH; FILAMENT WINDING; NUMERICAL METHODS; STRESSES;

AXIAL COMPRESSIVE LOADS; FILAMENT WOUND LATTICE STRUCTURES; LATTICE CYLINDERS; LATTICE SHELL; LAUNCH VEHICLES; OPTIMAL CONSTRAINT;

SPACE SHUTTLES;

EID: 0032683926     PISSN: 08931321     EISSN: None     Source Type: Journal    
DOI: 10.1061/(ASCE)0893-1321(1999)12:3(83)     Document Type: Article

References (7)

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2. Gramoll, K. C., Namiki, F, and Onoda, J. (1990a). "Dome thickness of filament wound pressure vessels." Trans., Japan Soc. for Aeronautical and Space Sci., 33(100), 66-79.
3. Gramoll, K. C., Namiki, F., and Onoda, J. (199Ob). "General structural analysis of an upper stage composite rocket motor case." Proc., 17th Int. Symp. of Space Technol. and Sci., 519-526.
4. Hosomura, T., Kaishima, T., and Mori, D. (1981). "New CFRP structural element." Proc., Japan-US Conf. on Composite Mat., 447-452.
5. Nakamura, T. (1988). "CFRP application to upper stage structure of Japan's launch vehicles." Proc., 4th Japan-US Conf. on Composite Mat., 923-932.
6. Nozaki, Y., Takamatsu, H., Fukushima, Y, and Matsubara, S. (1982). "Development of CFRP spacecraft attach fitting." Proc., 13th Int. Symp. on Space Technol. and Sci., 373-378.
7. Onoda, J. (1986). "An optimal design of lattice cylinder." Proc., JSASS/JSME 25th Struct. Conf., 46-62.