2011
DOI: 10.1016/j.icarus.2010.11.005
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In situ observation of penetration process in silica aerogel: Deceleration mechanism of hard spherical projectiles

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Cited by 24 publications
(22 citation statements)
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“…In the case of the penetration hole shown in Fig. 4a, the C d was determined to be about 0.9, a value almost consistent with those obtained for other porous materials such as aerogel and polyurethane foam, and the C d is 1.1 for aerogel, as obtained by Niimi et al (2011), and 0.9 for polyurethane foam, as obtained by Trucano and Grady (1995). In the case of a hemispherical cavity, we fit the data between 0 ls and 20 ls corresponding to t s of the cavity growth by using Eq.…”
Section: Drag Coefficients Of Projectilessupporting
confidence: 85%
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“…In the case of the penetration hole shown in Fig. 4a, the C d was determined to be about 0.9, a value almost consistent with those obtained for other porous materials such as aerogel and polyurethane foam, and the C d is 1.1 for aerogel, as obtained by Niimi et al (2011), and 0.9 for polyurethane foam, as obtained by Trucano and Grady (1995). In the case of a hemispherical cavity, we fit the data between 0 ls and 20 ls corresponding to t s of the cavity growth by using Eq.…”
Section: Drag Coefficients Of Projectilessupporting
confidence: 85%
“…(2) The drag coefficient, C d , could be estimated from the results of d by using an equation of projectile motion by Niimi et al (2011), and we found that the C d was 0.9 for a penetration hole, which was almost consistent with other porous materials such as aerogel, while the C d for a hemispherical cavity was 2.3-3.9, larger than that for a penetration hole because of the deformation and destruction of projectile. Furthermore, we could estimate the compressional strength of the target, Y ct , by using a stopping time, t s , assuming the shock pressure P = q t C t v i , and we found Y ct $ 400 MPa, that is, the projectile cannot penetrate the target after the shock pressure was attenuated to less than 400 MPa.…”
Section: Discussionsupporting
confidence: 55%
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“…Hypervelocity impact experiments on very low-density materials have been carried out to extend the cratering experiments (e.g., Cannon and Turner, 1967;Fechtig et al, 1980;Werle et al, 1981;Love et al, 1993;Trucano and Grady, 1995) and to develop and calibrate the instruments for intact capture of interplanetary dust samples using foams (e.g., Ishibashi et al, 1990;Tsou, 1990) and for aerogels (e.g., Barrett et al, 1992;Hörz et al, 1993Hörz et al, , 1998Hörz et al, , 2009Burchell et al, 1999Burchell et al, , 2001Burchell et al, , 2008Burchell et al, , 2009Kitazawa et al, 1999;Niimi et al, 2011Niimi et al, , 2012. These previous studies indicate that the impacts between high-density projectiles and low-density targets generate ''penetration tracks'': track diameter is small at the entrance (= impact point), then increases with depth, takes a peak, and decreases (this qualitative feature is common for any track).…”
Section: Introductionmentioning
confidence: 99%