Kopsavilkums
The SMART-1 end-of-life impact with the lunar surface was simulated with impacts in a two stage light-gas gun onto inclined basalt targets with a shallow surface layer of sand. This simulated the probable impact site, where a loose regolith will have overlaid a well consolidated basaltic layer of rock. The impact angles used were at 5° and 10° from the horizontal. The impact speed was ~2 km s-1 and the projectiles were 2.03 mm diameter aluminum spheres. The sand depth was between approximately 0.8 and 1.8 times the projectile diameter, implying a loose lunar surface regolith of similar dimensions to the SMART-1 spacecraft. A crater in the basement rock itself was only observed in the impact at 10° incidence, and where the depth of loose surface material was less than the projectile diameter, in which case the basement rock also contained a small pit-like crater. In all cases, the projectile ricocheted away from the impact site at a shallow angle. This implies that at the SMART-1 impact site the crater will have a complicated structure, with exposed basement rock and some excavated rock displaced nearby, and the main spacecraft body itself will not be present at the main crater.
| Oriģinālvaloda | Angļu |
|---|---|
| Lapas (no-līdz) | 1436-1448 |
| Lapu skaits | 13 |
| Žurnāls | Meteoritics and Planetary Science |
| Sējums | 50 |
| Izdevuma numurs | 8 |
| DOIs | |
| Publikācijas statuss | Publicēts - 1 aug. 2015 |
| Ārēji publicēts | Jā |
Nospiedums
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