Modeling of propellant leakage through matrix cracks in composite laminates

19th AIAA Applied Aerodynamics Conference

Volumn , Issue , 2001, Pages

  Kumazawa, Hisashi ^a   Aoki, Takahira ^b   Ishikawa, Takashi ^a   Susuki, Ippei ^a  

^a JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

^b UNIVERSITY OF TOKYO   (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; CARBON FIBER REINFORCED PLASTICS; COMPOSITE PROPELLANTS; CRACKS; CRYOGENICS; FIBER REINFORCED PLASTICS; MOLECULAR DYNAMICS; PROPELLANTS;

BIAXIALLY LOADED; CARBON FIBER REINFORCED PLASTICS (CFRP); CFRP LAMINATE; COMPOSITE LAMINATE; CRUCIFORM SPECIMENS; CRYOGENIC PROPELLANT TANKS; CRYOGENIC TEMPERATURES; THERMAL CONTRACTION;

LAMINATED COMPOSITES;

EID: 85067321060     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2001-1217     Document Type: Conference Paper

References (8)

1. T. Aoki, T. Ishikawa, H. Kumazawa and Y. Morino, "Mechanical Performance of CF/Polymer Composite Laminates under Cryogenic Conditions," AIAA paper, AIAA-2000-1605.
2. Marshall Space Flight Center - NASA, "Final Report of the X-33 Liquid Hydrogen Tank Test Investigation Team," May 2000.
3. S. Disdier, J. M. Rey, P. Pailler and A. R. Bun-sell, "Helium Permeation in Composite Materials for Cryogenic Application," Cryogenics, Vol. 38, 1998, pp.135-142.
4. C. Henaff-Gardin, M. C. Lafarie-Frenot and D. Gamby, "Doubly Periodic Matrix Cracking in Composite Laminates Part 1: General In-Plane Loading," Composite Structures, Vol. 36, 1996, pp.113-130.
5. D. H. Holkeboer, F. Pagano, D. W. Jones and D. J. Santeler, "Vacuum Engineering," Boston Technical Publishers, 1967.
6. T. Okada, S. Nishijima, K. Fujioka and Y. Ku-raoka, "Gas Permeation and Performance of an FRP Cryostat," Advances in Cryogenic Engineering, Vol. 34, 1988, pp. 17-24.
7. J. Humpenoder, "Gas Permeation of Fiber Reinforced Plastics," Cryogenics, Vol. 38, 1998, pp. 143-147.
8. M. J. Robinson, "Composite Cryogenic Propellant Tank Development," AIAA paper, AIAA-94-1375-CP.