Impurity profile and energy band diagram for the cuprous sulfide-cadmium sulfide heterojunction
Impurity profile and energy band diagram for cuprous sulfide-cadmium sulfide heterojunction
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Impurity profile and energy band diagram for cuprous sulfide-cadmium sulfide heterojunction
Copper sulfide-cadmium sulfide thin film solar cells under simulated orbital conditions, including thermal cycling, constant illumination and temperature effects
Open circuit and bias degradation tests in copper and cadmium sulfide thin film solar cells
Temperature-composition phase diagram of MnS- CdS binary system, noting solid solutions formation mechanisms
Thin-film Cu2S-CdS solar cells, loaded at various fixed values of load resistance, were thermally cycled for 1429 cycles in a simulated space environment. Cell performance was measured under controlled conditions in air before and after thermal cycling. These data were used to determine the effect of load voltage on cell performance. The performance of the cells was relatively independent of load voltage up to about 0.39 volt. This appears to be a threshold voltage, beyond which there was a significant loss in cell performance. Fortunately, this threshold voltage appears to be sufficiently higher than the maximum power voltage of 0.33 volt so that it can be avoided in most applications.
Cadmium sulfide films with larger than bandgap photovoltages, analyzing photovoltage decay and temperature and light intensity effects
Optical transmission characteristics of copper sulfide barriers formed on cadmium sulfide films
Cuprous sulfide layer on single crystal cadmium sulfide surface
Cadmium sulfide film cell photovoltaic effect and mechanism, discussing cell structure and spectral response
Cadmium sulfide (Cu2s - CdS) solar cells were tested under simulated space environmental conditions. Some cells were thermally cycled with illumination from a Xenon-arc solar simulator. A cycle was one hour of illumination followed immediately with one-half hour of darkness. In the light, the cells reached an equilibrium temperature of 60 C (333 K) and in the dark the cell temperature dropped to -120 C (153 K). Other cells were constantly illuminated with a Xenon-arc solar simulator. The equilibrium temperature of these cells was 55 C (328 K). The black vacuum chamber walls were cooled with liquid nitrogen to simulate a space heat sink. Chamber pressure was maintained at 0.000001 torr or less. Almost all of the solar cells tested degraded in power when exposed to a simulated space environment of either thermal cycling or constant illumination. The cells tested the longest were exposed to 10.050 thermal cycles.
A single crystal layer of either cadmium sulfide or an alloy of cadmium sulfide and indium phosphide is epitaxially deposited on a substrate of cadmium sulfide by liquid phase epitaxy using indium as the solvent.
Thermal neutron induced defects in cadmium sulfide and cadmium telluride
Explorer XIII satellite - cadmium sulfide experiment for micrometeoroid detection
Ultraviolet reflection spectrum of cadmium sulfide crystals
Impurity photovoltaic effect in cadmium sulfide, noting radiative enhancement of spectral response upon illumination with green light
Cadmium sulfide thin film photovoltaic cells - cadmium sulfide film evaporation, cell testing, improvement, and stability, and plastic and metal substrate cells
The design, development, fabrication and tests of flexible integrated thin-film cadmium sulfide solar cells and modules are discussed. The development of low cost and high production rate methods for interconnecting cells into large solar arrays is described. Chromium thin films were applied extensively in the deposited cell structures as a means to: (1) achieve high adherence between the cadmium sulfide films and the vacuum-metallized copper substrates, (2) obtain an ohmic contact to the cadmium sulfide films, and (3) improve the adherence of gold films as grids or contact areas.