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Volumn 33, Issue 1-12, 2006, Pages 855-861

Hypervelocity impact tests on coated thermoplastic films at cryogenic and elevated temperatures

Author keywords

Cryogenic; Hypervelocity; Kapton

Indexed keywords

COATED MATERIALS; IMPACT TESTING; THERMOPLASTICS;

EID: 33845187795     PISSN: 0734743X     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.ijimpeng.2006.09.033     Document Type: Article
Times cited : (12)

References (6)
  • 1
    • 33845209991 scopus 로고    scopus 로고
    • Perrygo C, Parrish K, Wooldridge E. Sunshield meteoroid impact test and analysis requirement definition, NASA internal document, 1999.
  • 2
    • 2342507764 scopus 로고    scopus 로고
    • Temperature effects on bumper hole diameter for impact velocities from 2 to 7 km/s
    • Myers B.A., Schonberg W.P., and Williamson J.E. Temperature effects on bumper hole diameter for impact velocities from 2 to 7 km/s. Int J Impact Eng 29 (2003) 487-495
    • (2003) Int J Impact Eng , vol.29 , pp. 487-495
    • Myers, B.A.1    Schonberg, W.P.2    Williamson, J.E.3
  • 3
    • 33845217190 scopus 로고    scopus 로고
    • Wells B.K., Cryogenic and elevated temperature hypervelocity impact facility, In: Hyper velocity impact symposium, 2005, Lake Tahoe, CA.
  • 4
    • 33845219432 scopus 로고    scopus 로고
    • Coombs C., Watts A., Wagner J., Atkinson D., LDEF data: Comparison with existing models, In: LDEF-69 months in space, second LDEF post retrieval symposium, vol. 2, 1992, p. 619-64.
  • 5
    • 33845197330 scopus 로고    scopus 로고
    • Coombs C., Atkinson D., Allbrooks M., Watts A., Hennessy C., Wagner J., Danger areas on selected LDEF aluminum surfaces. In: LDEF-69 months in space, second LDEF post retrieval symposium, vol. 2, 1992, p. 595-618.


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.