Production and Impact Characterization of Enceladus Ice Grain Analogues

被引:13
作者
Miller, Morgan E. C. [1 ,2 ]
Burke, Sally E. [1 ]
Continetti, Robert E. [1 ]
机构
[1] Univ Calif San Diego, Dept Nanoengn, La Jolla, CA 92093 USA
[2] Thermo Fisher Sci, San Jose, CA 95134 USA
来源
ACS EARTH AND SPACE CHEMISTRY | 2022年
基金
美国国家航空航天局;
关键词
scattering dynamics; aerosol impact spectrometer; tapered image charge detector; Enceladus; hypervelocity; evaporative cooling; radiative heating; E-RING; WATER; PLUME;
D O I
10.1021/acsearthspacechem.2c00087
中图分类号
O6 [化学];
学科分类号
0703 ;
摘要
Experiments examining the production of Enceladus ice grain analogues and the characterization of their impact phenomena are reported. These measurements make use of a unique single particle accelerator-the aerosol impact spectrometer (AIS)-to extend studies of the impact dynamics of ice grains down to the 0.1-10 mu m diameter range relevant to orbital sampling of Enceladus ice grains. Laboratory generation of Enceladus plume grains followed by an examination of their impact dynamics is required to support the interpretation of ice grain orbital sampling in a potential flyby mission concept. In the work reported here, the AIS was used to inject charged water droplets produced in an electrospray ionization source through an aerodynamic lens and into vacuum such that they freeze within 50-200 mu s. The ice grains were then accelerated to a controlled final velocity using a linear accelerator (LINAC). The capability of the LINAC to achieve hypervelocity speeds is explored here. The AIS was equipped with the tapered image charge detector, a multielement image charge detector composed of three charge-sensitive rings and the collision analysis target, providing angle-resolved measurements that revealed impact phenomena including rebound, sticking, and fragmentation for ice grain impacts on a molybdenum target. The velocity-dependent trends of these impact phenomena are reported for impacts ranging from 20 to 900 m/s.
引用
收藏
页码:1813 / 1822
页数:10
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