메뉴 건너뛰기




Volumn 19, Issue 1, 1998, Pages 65-70

The gradient of mechanical characteristics across the thickness of composite laminates after exposure to a low earth orbit environment

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT MATERIALS; CARBON FIBER REINFORCED PLASTICS; ELASTIC MODULI; EPOXY RESINS; GLASS FIBER REINFORCED PLASTICS; GLASS TRANSITION; LAMINATED COMPOSITES; MICROHARDNESS; SPACECRAFT; THERMAL CYCLING; THERMAL EXPANSION; COMMUNICATION SATELLITES; DILATOMETERS; DYNAMIC MECHANICAL ANALYSIS; DYNAMICS; ELASTOMERS; FIBER REINFORCED PLASTICS; GLASS; LAMINATES; MECHANICAL PROPERTIES; ORBITS;

EID: 0031988207     PISSN: 02728397     EISSN: None     Source Type: Journal    
DOI: 10.1002/pc.10076     Document Type: Article
Times cited : (11)

References (7)
  • 4
    • 11644262702 scopus 로고
    • Investigation of PCM at Long-Term Exposure to Space Environment
    • Batumi, Russia
    • Research Report, "Investigation of PCM at Long-Term Exposure to Space Environment," Batumi, Russia (1991).
    • (1991) Research Report
  • 5
    • 5344258202 scopus 로고
    • Forecast of Stability of Composite Materials, Applied for Micrometeor Protection
    • Research Institute of Ecological Monitoring at ASU, "Satyut" Design Office, Barnaul, Russia
    • Research Report No. 1-18/94, 1994, "Forecast of Stability of Composite Materials, Applied for Micrometeor Protection," Research Institute of Ecological Monitoring at ASU, "Satyut" Design Office, Barnaul, Russia (1995).
    • (1995) Research Report No. 1-18/94, 1994


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.