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Volumn 47, Issue 1-2, 1999, Pages 103-115

Modeling damage in spacecraft impacted by orbital debris particles

Author keywords

[No Author keywords available]

Indexed keywords

HAZARDS; MATHEMATICAL MODELS; ORBITS; REGRESSION ANALYSIS; SPACE DEBRIS; CRACKS; EARTH (PLANET); MANNED SPACE FLIGHT; SPACE STATIONS;

EID: 0032600933     PISSN: 00219142     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article
Times cited : (2)

References (6)
  • 1
    • 3042924395 scopus 로고
    • Vulnerability of manned spacecraft to crew loss from orbital debris penetration
    • Alabama
    • WILLIAMSEN, J. E. "Vulnerability of Manned Spacecraft to Crew Loss from Orbital Debris Penetration," NASA-TM-108452, Marshall Space Flight Center, Alabama, 1994.
    • (1994) NASA-TM-108452, Marshall Space Flight Center
    • Williamsen, J.E.1
  • 2
    • 0031376534 scopus 로고    scopus 로고
    • Empirical hole and crack length models for dual-wall systems under hypervelocity projectile impact
    • SCHONBERG, W. P. and WILLIAMSEN, J. E. "Empirical Hole and Crack Length Models for Dual-Wall Systems Under Hypervelocity Projectile Impact," International Journal of Impact Engineering, Vol. 20, 1997, pp.711-722.
    • (1997) International Journal of Impact Engineering , vol.20 , pp. 711-722
    • Schonberg, W.P.1    Williamsen, J.E.2
  • 3
    • 0042257760 scopus 로고
    • Multi-plate damage study
    • Elgin AFB, Florida
    • BURCH, G. T. "Multi-Plate Damage Study," AFATL-TR-67-116, Elgin AFB, Florida, 1967.
    • (1967) AFATL-TR-67-116
    • Burch, G.T.1
  • 4
    • 0031142276 scopus 로고    scopus 로고
    • Cracking characteristics of dual-wall structures following simulated orbital debris particle impact
    • SCHONBERG, W. P. and WILLIAMSEN, J. E. "Cracking Characteristics of Dual-Wall Structures Following Simulated Orbital Debris Particle Impact," Journal of Spacecraft and Rockets, Vol. 34, No. 3, 1997, pp. 318-324.
    • (1997) Journal of Spacecraft and Rockets , vol.34 , Issue.3 , pp. 318-324
    • Schonberg, W.P.1    Williamsen, J.E.2
  • 5
    • 0029710654 scopus 로고    scopus 로고
    • Space station module wall hole size and crack length following an orbital debris penetration of 6.5 km/s
    • Albuquerque, New Mexico
    • SCHONBERG, W. P. and WILLIAMSEN, J. E. "Space Station Module Wall Hole Size and Crack Length Following an Orbital Debris Penetration of 6.5 km/s," proceedings of the SPACE 96/Comet Day II Symposium, Vol. 1, pp. 1-7, Albuquerque, New Mexico, 1996.
    • (1996) Proceedings of the SPACE 96/Comet Day II Symposium , vol.1 , pp. 1-7
    • Schonberg, W.P.1    Williamsen, J.E.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.