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Hole size and crack length models for spacecraft walls under oblique hypervelocity projectile impact

Research output: Contribution to journalArticlepeer-review

Original languageEnglish
Pages (from-to)461-471
Number of pages11
JournalAerospace Science and Technology
Volume3
Issue number7
DOIs
StatePublished - Oct 1999

ASJC Scopus Subject Areas

  • Aerospace Engineering

Keywords

  • Crack propagation
  • Hypervelocity impact
  • Orbital debris
  • Spacecraft survivability

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