Thermal distortion analysis of orbiting solar array including degradation effects of composite materials

Composites Part B:Engineering

Volumn 32, Issue 4, 2001, Pages 271-285

  Shin, Kwang Bok ^a   Kim, Chun Gon ^a   Hong, Chang Sun ^a   Lee, Ho Hyung ^b  

^a Korea Advanced Institute of Science and Technology (KAIST)   (South Korea)

^b Korea Aerospace Research Institute (KARI)   (South Korea)

Author keywords

Composite material

Indexed keywords

COMPUTER SIMULATION; DEGRADATION; HONEYCOMB STRUCTURES; SANDWICH STRUCTURES; SOLAR CELL ARRAYS; STRUCTURAL PANELS; TEMPERATURE DISTRIBUTION; THERMAL CYCLING; ULTRAVIOLET RADIATION;

COMPOSITE FACESHEETS; THERMAL DISTORTION ANALYSIS;

COMPOSITE MATERIALS;

EID: 0035001527     PISSN: 13598368     EISSN: None     Source Type: Journal    
DOI: 10.1016/S1359-8368(01)00020-8     Document Type: Article

References (13)

1. Effects of space environmental conditions on graphite epoxy composites
2. Self-shadowing effects on the thermal-structural response of orbiting trusses
3. Solar-array-induced disturbance of the hubble space telescope pointing system
4. Low earth orbit effects on organic composites flown on the long duration exposure facility
5. TRASYS Modeling and Thermal Analysis of KOMPSAT
6. Prediction of failure thermal cycles in graphite/epoxy composite materials under simulated low earth orbit environments
7. Toughened graphite/epoxy composite exposed in near-earth orbit for 5.8 years
8. Space environmental effects on graphite/epoxy composites