Design, damage tolerance and filament wound attach fitting for launch vehicle

Journal of Advanced Materials

Volumn 30, Issue 1, 1998, Pages 16-21

  Hou, An ^a   Gramoll, Kurt ^a  

^a Georgia Institute of Technology   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE VEHICLES; BUCKLING; CARBON FIBER REINFORCED PLASTICS; COMPRESSIVE STRESS; FAILURE ANALYSIS; SHELLS (STRUCTURES); STRENGTH OF MATERIALS; STRESS ANALYSIS; STRUCTURAL ANALYSIS;

LATTICE STRUCTURES;

FILAMENT WINDING;

EID: 0031617587     PISSN: 10709789     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

References (10)

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3. Y. Nozaki, H. Takamatsu, Y. Fukushima, and S. Matsubara, "Development of CFRP Spacecraft Attach Fitting," Proceedings of the Thirteenth International Symposium on Space Technology and Science, Tokyo, pp. 373-378 (1982).
4. Y. Fukushima, T. Nakamura, H. Shirogan, T. Endo, and S. Yamashita, 1986, "The Development of Upper Stage Structures," Proceedings of the Fifteenth International Symposium on Space Technology and Science, Tokyo, pp. 431-436 (1986).
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6. K.C. Gramoll, F. Namiki, and J. Onoda, "Dome Thickness of Filament Wound Pressure Vessels," Transactions of Japan Society for Aeronautical and Space Sciences, Vol. 33, No. 100, pp. 66-79 (1990).
7. K.C. Gramoll, F. Namiki, and J. Onoda, "General Structural Analysis of an Upper Stage Composite Rocket Motor Case," Proc. of the Seventeenth International Symposium of Space Technology and Science, Tokyo, Japan, pp. 519-526 (1990).
8. T. Hayashi, "Buckling Strength of Cylindrical Geodesic Structures," Japan-US Conference on Composite Materials, Tokyo, pp. 428-438 (1981).
9. th Structures Conference, pp. 46-62 (1986).
10. L.W. Rehfield and R.B. Deo, "Continuous Filament Advanced Composite Isogrid A Promising Structural Concept," Fibrous Composites in Structural Design, Edited by Edward M. Lenoe, pp. 215-235.