Thermal/mechanical response and damage growth in polymeric composites at cryogenic temperatures

Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference

Volumn 3, Issue , 2002, Pages 1677-1689

  Whitley, Karen S ^a   Gates, Thomas S ^a  

^a NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT FUEL TANKS; CRYOGENICS; DEGRADATION; ELASTIC MODULI; LAMINATED COMPOSITES; RESIDUAL STRESSES; STRAIN; TENSILE STRENGTH;

POLYMERIC COMPOSITES;

CARBON FIBER REINFORCED PLASTICS;

EID: 0036072669     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2002-1416     Document Type: Conference Paper

References (16)

1. Feasibility study of CFRP material application to the cryogenic propellant tank of reusable launch vehicles
2. Composite cryogenic propellant tank development
3. Composite structures on the DC-XA reusable launch vehicle
4. Use of resin composites for cryogenic tankage
5. Fatigue properties of unidirectional carbon fiber composites at cryogenic temperatures
6. Durability of carbon fibre reinforced plastics with thermoplastic matrices under cyclic mechanical and cyclic thermal loads at cryogenic temperatures
7. Cryogenic mechanical response of carbon fibre reinforced plastics with thermoplastic matrices to quasi-static loads
8. Properties of composite materials for cryogenic applications
9. Steady state cracking of PMC's at cryogenic temperatures
10. Study of CFRP application to the cryogenic propellant tank of reusable launch vehicle
11. Temperature polyimide materials in extreme temperature environments