NASA NTRS ยท 19780019229
Particle impact tests
Abstract
Particle impact tests were performed on three types of orbiter surface with a micrometeoroid facility. The test equipment electrostatically accelerated micron sized particles to high velocities simulating micrometeoroid impacts. Test particles were titanium diboride with typical velocities in the range 1 to 2.3 km x sec/1 and equivalent particle diameters in the range 4 to 16 microns. Impact angles to the material surface were 90, 60 and 30 degrees. The particle impact sites were located on the sample surfaces and craters were photographed with a magnification of 400X.
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Komatsu, G. K.. 1978-05-01. Particle impact tests. https://ntrs.nasa.gov/citations/19780019229
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