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Volumn 23, Issue 1 PART I, 1999, Pages 125-136

Flexible and deployable meteoroid/debris shielding for spacecraft

Author keywords

[No Author keywords available]

Indexed keywords

BALLISTICS; FABRICS; FOAMED PLASTICS; IMPACT TESTING; POLYURETHANES; SHIELDING; SPACE DEBRIS; SPACECRAFT;

EID: 0033361707     PISSN: 0734743X     EISSN: None     Source Type: Journal    
DOI: 10.1016/s0734-743x(99)00068-8     Document Type: Article
Times cited : (60)

References (10)
  • 2
    • 84880840745 scopus 로고    scopus 로고
    • Presentedto the NASA Johnson Space Director, May 1997 and the NASA Administrator, July
    • W.C. Schneider et al., Mars TransHab Design Study Team (executive summary), Presented to the NASA Johnson Space Director, May 1997 and the NASA Administrator, July 1997.
    • (1997) Mars TransHab Design Study Team (Executive Summary)
    • Schneider, W.C.1
  • 4
    • 0003183430 scopus 로고
    • A Multi-Shock Concept for Spacecraft Shielding
    • B.G. Cour-Palais and J.L. Crews, A Multi-Shock Concept for Spacecraft Shielding, Int. J. Impact Engng, Vol. 10, pp. 135-146 (1990).
    • (1990) Int. J. Impact Engng , vol.10 , pp. 135-146
    • Cour-Palais, B.G.1    Crews, J.L.2
  • 7
    • 0027284636 scopus 로고
    • Design and Performance Equations for Advanced Meteoroid and Debris Shields
    • E.L. Christiansen, Design and Performance Equations for Advanced Meteoroid and Debris Shields, Int. J. Impact Engng, Vol.14, pp.145-156 (1993).
    • (1993) Int. J. Impact Engng , vol.14 , pp. 145-156
    • Christiansen, E.L.1
  • 8
    • 33646270107 scopus 로고    scopus 로고
    • NASA Johnson Space Center (JSC) Hypervelocity Impact Technology Facility (HITF), Web Page, http://hitf.jsc.nasa.gov/


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.