A metal oxide film includes indium, M, (M is Al, Ga, Y, or Sn), and zinc and includes a region where a peak having a diffraction intensity derived from a crystal structure is observed by X-ray diffraction in the direction perpendicular to the film surface. Moreover, a plurality of crystal parts is observed in a transmission electron microscope image in the direction perpendicular to the film surface. The proportion of a region other than the crystal parts is higher than or equal to 20% and lower than or equal to 60%.

A composite ceramic including: a lithium garnet major phase; and a grain growth inhibitor minor phase, as defined herein. Also disclosed is a method of making composite ceramic, pellets and tapes thereof, a solid electrolyte, and an electrochemical device including the solid electrolyte, as defined herein.

A dielectric ceramic composition includes main component grains having a perovskite structure represented by a formula AMO.sub.3. “A” includes Ba. “M” includes Ti. The dielectric ceramic composition includes a 4A subcomponent. The 4A subcomponent includes Fe and Mn. A molar ratio of Mn to a total of Fe and Mn in terms of a metal element is 0.18 to 0.65.

Disclosed herein are embodiments of an enhanced resonant frequency hexagonal ferrite material and methods of manufacturing. The hexagonal ferrite material can be Y-phase strontium hexagonal ferrite material. In some embodiments, sodium can be added into the crystal structure of the hexagonal ferrite material in order to achieve high resonance frequencies while maintaining high permeability.

A sintered oxide contains In element, Y element, and Ga element at respective atomic ratios as defined in formulae (1) to (3) below,

0.80≤In/(In+Y+Ga)≤0.96  (1),

0.02≤Y/(In+Y+Ga)≤0.10  (2), and

0.02≤Ga/(In+Y+Ga)≤0.10  (3), and

Al element at an atomic ratio as defined in a formula (4) below,

0.005≤Al/(In+Y+Ga+Al)≤0.07  (4),

where In, Y, Ga, and Al in the formulae represent the number of atoms of the In element, Y element, Ga element, and Al element in the sintered oxide, respectively.

A spark plug connecting element. The spark plug connecting element includes a first contact element and a second contact element. A resistor element is situated between the first contact element and the second contact element. The first contact element and the second contact element have a specific conductivity of 10.sup.2 S/m to 10.sup.8 S/m and the resistor element has a specific conductivity of 10.sup.−3 S/m to 10.sup.1 S/m.

A composite ceramic including: a lithium garnet major phase; and a grain growth inhibitor minor phase, as defined herein. Also disclosed is a method of making composite ceramic, pellets and tapes thereof, a solid electrolyte, and an electrochemical device including the solid electrolyte, as defined herein.

A refractory article includes a body including a ceramic having an aluminosilicate present in an amount of at least 70 wt % and not greater than 99 wt % for a total weight of the body, and the body further includes a dopant including a Mg-containing oxide compound and a Fe-containing oxide compound, and the dopant is present in an amount within a range including at least 1 wt % and not greater than 12 wt %.

A sintered composite ceramic, including: a lithium-garnet major phase; and a grain growth inhibitor minor phase, such that the grain growth inhibitor minor phase has a metal oxide in a range of 0.1 wt. % to 10 wt. % based on the total weight of the sintered composite ceramic.

The present invention relates to an innovative thermal design concept of tailoring the absorptance and emittance of a coating—namely silicon oxide (SiOx) coated aluminized Kapton—as a radiator coating for small, nano-satellite (i.e., CubeSat) thermal management. The present invention improves on the thermal design of existing satellites, by: a) thermally coupling all components to the baseplate to eliminate the need for heater power for the battery; b) using all six sides of the CubeSat as radiators by changing the wall material from fiberglass to aluminum; c) using a different ratio of absorptance to emittance for each side by tailoring the SiO.sub.x thickness; d) having a high emittance for the wall interior and components; and e) eliminating the need for MLIs. The elimination of the MLIs reduces the volume and increases the clearance to minimize the risk for solar array deployment and cost of the thermal control subsystem.