| タイトル | Particle impact tests |
| 本文（外部サイト） | http://hdl.handle.net/2060/19780019229 |
| 著者（英） | Komatsu, G. K. |
| 著者所属（英） | TRW Defense and Space Systems Group |
| 発行日 | 1978-05-01 |
| 言語 | eng |
| 内容記述 | 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. |
| NASA分類 | SPACECRAFT PROPULSION AND POWER |
| レポートNO | 78N27172
NASA-CR-151739
TRW-32970-6001-RU-00 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/178418 |
