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Volumn 29, Issue 1-10, 2003, Pages 691-702

Hypervelocity impact on spacecraft honeycomb: Hydrocode simulation and damage laws

Author keywords

AUTODYN; Ballistic limit; Damage laws; Debris; Honeycomb; Hydrocode; Hypervelocity; Spacecraft; Structure

Indexed keywords

ALUMINUM; BALLISTICS; COMPUTER SIMULATION; HONEYCOMB STRUCTURES; HYDRODYNAMICS; SPACE DEBRIS;

EID: 2342507732     PISSN: 0734743X     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.ijimpeng.2003.10.016     Document Type: Conference Paper
Times cited : (65)

References (14)
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  • 5
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  • 7
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    • The characteristics of penetration for a double-sheet structure with honeycomb
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    • (1970) NASA TM , vol.X-53974
    • Jex, D.W.1    Miller, A.M.2    Mackay, C.A.3
  • 12
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    • Hole growth characterisation for hypervelocity impacts in thin targets
    • Gardner DJ, McDonnell JAM, Collier I. Hole growth characterisation for hypervelocity impacts in thin targets. Int. J. Impact Engng., 1997; 19(7): 589-602.
    • (1997) Int. J. Impact Engng. , vol.19 , Issue.7 , pp. 589-602
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.