Test procedures to evaluate spacecraft materials ejecta upon hypervelocity impact

Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering

Volumn 221, Issue 6, 2007, Pages 969-974

  Siguier, J M ^a   Mandeville, J C ^a  

^a ONERA   (France)

Author keywords

Ejecta; Hypervelocity impact; Micrometeoroids; Orbital debris; Spacecraft materials

Indexed keywords

DATABASE SYSTEMS; MATHEMATICAL MODELS; PARAMETER ESTIMATION; SPACE DEBRIS;

HYPERVELOCITY IMPACT; MICROMETEOROIDS; SPACECRAFT MATERIALS;

SPACECRAFT EQUIPMENT;

EID: 44449123652     PISSN: 09544100     EISSN: None     Source Type: Journal    
DOI: 10.1243/09544100JAERO236     Document Type: Article

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