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Impact Cratering Theory and Modeling for the Deep Impact Mission: From Mission Planning to Data Analysis

Authors :
Elisabetta Pierazzo
H. Jay Melosh
Natasha A. Artemeiva
James E. Richardson
Source :
Deep Impact Mission: Looking Beneath the Surface of a Cometary Nucleus ISBN: 1402035993
Publication Year :
2006
Publisher :
Springer-Verlag, 2006.

Abstract

The cratering event produced by the Deep Impact mission is a unique experimental opportunity, beyond the capability of Earth-based laboratories with regard to the impacting energy, target material, space environment, and extremely low-gravity field. Consequently, impact cratering theory and modeling play an important role in this mission, from initial inception to final data analysis. Experimentally derived impact cratering scaling laws provide us with our best estimates for the crater diameter, depth, and formation time: critical in the mission planning stage for producing the flight plan and instrument specifications. Cratering theory has strongly influenced the impactor design, producing a probe that should produce the largest possible crater on the surface of Tempel 1 under a wide range of scenarios. Numerical hydrocode modeling allows us to estimate the volume and thermodynamic characteristics of the material vaporized in the early stages of the impact. Hydrocode modeling will also aid us in understanding the observed crater excavation process, especially in the area of impacts into porous materials. Finally, experimentally derived ejecta scaling laws and modeling provide us with a means to predict and analyze the observed behavior of the material launched from the comet during crater excavation, and may provide us with a unique means of estimating the magnitude of the comet’s gravity field and by extension the mass and density of comet Tempel 1.

Details

ISBN :
978-1-4020-3599-9
1-4020-3599-3
ISBNs :
9781402035999 and 1402035993
Database :
OpenAIRE
Journal :
Deep Impact Mission: Looking Beneath the Surface of a Cometary Nucleus ISBN: 1402035993
Accession number :
edsair.doi...........2a7aea3cb473bca9694a9011eb09f801
Full Text :
https://doi.org/10.1007/1-4020-4163-2_10