Applicability of CFRP materials to the cryogenic propellant tank for reusable launch vehicle (RLV)

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

Volumn 10, Issue 4, 2001, Pages 339-347

  Morino, Y ^a   Shimoda, T ^a   Morimoto, T ^a   Ishikawa, T ^a   Aoki, T ^a  

^a JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

Author keywords

Composites; Cryogenic tank; RLV

Indexed keywords

COMPOSITE STRUCTURES; CRYOGENIC EQUIPMENT; CRYOGENICS; MATERIALS TESTING; MODEL STRUCTURES; PLASTIC BUILDING MATERIALS; PROPELLANTS; TANKS (CONTAINERS);

REUSABLE LAUNCH VEHICLE; WEIGHT REDUCTION;

CARBON FIBER REINFORCED PLASTICS;

EID: 0035574262     PISSN: 09243046     EISSN: None     Source Type: Journal    
DOI: 10.1163/156855101753415364     Document Type: Article

References (3)

1. CFRP material characterization testing for the RLV cryogenic propellant tank
2. Mechanical performance of CF/polymer composite laminates under cryogenic conditions
3. Feasibility study of the cryogenic composite tank for reusable launch vehicles