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Volumn 20, Issue 6-10, 1997, Pages 711-722

Empirical hole size and crack length models for dual-wall systems under hypervelocity projectile impact

Author keywords

[No Author keywords available]

Indexed keywords

CRACKS; MATHEMATICAL MODELS; MECHANICS; SPACE FLIGHT;

EID: 0031376534     PISSN: 0734743X     EISSN: None     Source Type: Journal    
DOI: 10.1016/s0734-743x(97)87457-x     Document Type: Article
Times cited : (41)

References (15)
  • 3
    • 0042257760 scopus 로고
    • AFATL-TR-67-116, Eglin Air Force Base, Florida
    • G. T. Burch, Multi-plate Damage Study. AFATL-TR-67-116, Eglin Air Force Base, Florida (1967).
    • (1967) Multi-plate Damage Study
    • Burch, G.T.1
  • 5
    • 38249010150 scopus 로고
    • Aluminum 2219-T87 vs. 5456-H116: A comparative study of pressure wall materials in dual-wall structures under hypervelocity impact
    • W. P. Schonberg, Aluminum 2219-T87 vs. 5456-H116: A Comparative Study of Pressure Wall Materials in Dual-Wall Structures Under Hypervelocity Impact. Acta Astronautica, 26, 799-812 (1992).
    • (1992) Acta Astronautica , vol.26 , pp. 799-812
    • Schonberg, W.P.1
  • 6
  • 9
    • 0030385035 scopus 로고    scopus 로고
    • Cracking characteristics of multi-wall pressure vessels following hypervelocity projectile impact
    • edited by Y. S. Shin and J. A. Zukas, Montreal, Canada
    • W. P. Schonberg and J. E. Williamsen, Cracking Characteristics of Multi-Wall Pressure Vessels Following Hypervelocity Projectile Impact. Proc. 1996 ASME Conference on Structures Under Extreme Loading Conditions, (edited by Y. S. Shin and J. A. Zukas), Montreal, Canada, AMSE-PVP-Vol. 325. (1996).
    • (1996) Proc. 1996 ASME Conference on Structures Under Extreme Loading Conditions , vol.325 AMSE-PVP
    • Schonberg, W.P.1    Williamsen, J.E.2
  • 10
    • 0029710654 scopus 로고    scopus 로고
    • Space station module wall hole size and crack length following an orbital debris penetration at 6.5 km/s
    • edited by S. E. Johnson, Albuquerque, New Mexico
    • W. P. Schonberg and J. E. Williamsen, Space Station Module Wall Hole Size and Crack Length Following an Orbital Debris Penetration at 6.5 km/s. Proc. SPACE 96/Comet Day II Symposium, Vol. I. (edited by S. E. Johnson), pp. 1-7, Albuquerque, New Mexico (1996).
    • (1996) Proc. SPACE 96/Comet Day II Symposium, Vol. I , vol.1 , pp. 1-7
    • Schonberg, W.P.1    Williamsen, J.E.2
  • 11
    • 3042969252 scopus 로고    scopus 로고
    • Hole size and crack length following orbital debris penetration of space station module walls at 6.5 and 11.3 km/s
    • edited by Y. Arakawa, Paper No. 96-m-20v, Gifu, Japan
    • W. P. Schonberg and J. E. Williamsen, Hole Size and Crack Length Following Orbital Debris Penetration of Space Station Module Walls at 6.5 and 11.3 km/s. Proc. 20th International Symposium on Space Technology and Science, (edited by Y. Arakawa), Paper No. 96-m-20v, Gifu, Japan (1996).
    • (1996) Proc. 20th International Symposium on Space Technology and Science
    • Schonberg, W.P.1    Williamsen, J.E.2
  • 13
    • 0027284636 scopus 로고
    • Design and perforation equations for advanced meteoroid and debris shields
    • E. L. Christiansen, Design and Perforation Equations for Advanced Meteoroid and Debris Shields. International Journal of Impact Engineering. 14, 145-156 (1992).
    • (1992) International Journal of Impact Engineering , vol.14 , pp. 145-156
    • Christiansen, E.L.1
  • 14
    • 30244552412 scopus 로고
    • Private Communication
    • E. L. Christiansen, Private Communication (1995).
    • (1995)
    • Christiansen, E.L.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.