The treatment of the problems due to hypervelocity impact during a fast fly-by (57 s) of Halley's comet

Physics

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Finite Difference Theory, Flyby Missions, Halley'S Comet, Hypervelocity Impact, Meteoroid Hazards, Spacecraft Shielding, Comet Nuclei, Micrometeoroids, Penetration, Space Probes, Spacecraft Design, Terminal Ballistics

Scientific paper

The problem of hypervelocity-impact at 57 km/sec during the fast flyby of Halley's comet is discussed. The possibilities of numerical analyses by the use of explicit finite-difference codes, the experimental techniques, and the behavior of materials under these conditions are briefly described. Based on an extrapolation of existing data, some characteristics of the bumper-layout are discussed. It is shown that additional data may be required to optimize the design of the bumper.

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