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SMART-1 end of life shallow regolith impact simulations

  • M. J. Burchell*
  • , M. J. Cole
  • , N. K. Ramkissoon
  • , P. J. Wozniakiewicz
  • , M. C. Price
  • , B. Foing
  • *Šī darba korespondējošais autors
  • University of Kent
  • The Natural History Museum, London
  • European Space Research and Technology Centre (ESTEC)

Zinātniskās darbības rezultāts: Devums žurnālamZinātniskais raksts (žurnālā)koleģiāli recenzēts

11 Atsauces (Scopus)

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.

OriģinālvalodaAngļu
Lapas (no-līdz)1436-1448
Lapu skaits13
ŽurnālsMeteoritics and Planetary Science
Sējums50
Izdevuma numurs8
DOIs
Publikācijas statussPublicēts - 1 aug. 2015
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