Publication Date:
2019-06-27
Description:
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.
Keywords:
SPACE SCIENCES
Type:
NASA-TN-D-6596
,
MSC-S-273
Format:
application/pdf
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