NASA NTRS ยท 19720012228
A guide to using meteoroid-environment models for experiment and spacecraft design applications
Abstract
A method was derived for transforming a meteoroid flux, defined relative to the earth and expressed as a function of meteoroid mass, velocity, and mass density into a meteoroid flux expressed as a function of penetration thickness (or some other parameter) on a moving spacecraft at some particular distance from the earth. The procedure for performing the transformation is summarized and an example is discussed.
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Kessler, D. J.. 1972-03-01. A guide to using meteoroid-environment models for experiment and spacecraft design applications. https://ntrs.nasa.gov/citations/19720012228
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