Cryogenic mechanical properties of CF/polymer composites for tanks of reusable rockets

Advanced Composite Materials: The Official Journal of the Japan Society of Composite Materials

Volumn 10, Issue 4, 2001, Pages 349-356

  Aoki, T ^a   Ishikawa, T ^a   Kumazawa, H ^a   Morino, Y ^a  

^a UNIVERSITY OF TOKYO   (Japan)

Author keywords

Cryogenics; Delamination; Interlaminar fracture toughness; Matrix crack; Mechanical properties; Propellant tank

Indexed keywords

CARBON FIBERS; CRACK PROPAGATION; CRYOGENICS; DELAMINATION; FRACTURE TOUGHNESS; ORGANIC POLYMERS; REUSABLE ROCKETS; TANKS (CONTAINERS); TENSILE STRENGTH; TENSILE STRESS;

MATRIX CRACK; REUSABLE LAUNCH VEHICLES;

CARBON FIBER REINFORCED PLASTICS;

EID: 0035573554     PISSN: 09243046     EISSN: None     Source Type: Journal    
DOI: 10.1163/156855101753415373     Document Type: Article

References (3)

1. Cryogenic properties of unidirectional composites
2. Delamination energy release rates under thermal loading in fiber-reinforced composite laminates
3. Thermally induced damages in composite laminates: Predictive methodology and experimental investigation