For many years extending solar power missions far from the sun has been a challenge not only due to the rapid falloff in solar intensity (intensity varies as inverse square of solar distance) but also because some of the solar cells in an array may exhibit a LILT (low intensity low temperature) degradation that reduces array performance. Recent LILT tests performed on commercial triple junction solar cells have shown that high performance can be obtained at solar distances as great as approx. 5 AU1. As a result, their use for missions going far from the sun has become very attractive. One additional question that remains is whether the radiation damage experienced by solar cells under low temperature conditions will be more severe than when...
GaAlAs/GaAs heteroface solar cells used in space offer advantages of higher operating temperatures a...
The motivation for advanced solar cell flight experiments is discussed and the Advanced Solar Cell O...
Solar array design for any spacecraft is determined by the orbit parameters. For example, operationa...
A series of environmental tests were completed on one type of triple junction a-Si and two types of ...
The degradation of solar cells under irradiation by high energy particles (electrons, protons) is th...
An analysis of the effects of low energy proton irradiation on the electrical performance of triple ...
The vast majority of space probes to date have relied upon photovoltaic power generation. If future ...
NASA missions such as DAWN and JUNO, as well as the planned Europa Clipper mission, rely on solar po...
We investigated the effects of irradiation beam conditions on the performance degradation of silicon...
International audienceTo understand the influence of proton irradiation on lattice‐matched GaInP/GaA...
The Power Extension Package (PEP) is the prime focus of a development program to produce low cost so...
One of the major limitations of solar cells in space power systems is their vulnerability to radiati...
The results of an experimental evaluation of the real-time degradation characteristics of lithium-di...
The results of post-flight performance testing of the solar cells flown on the Advanced Photovoltaic...
Latest results of 3G28 triple-junction solar cells manufactured by AZUR SPACE Solar Power GmbH under...
GaAlAs/GaAs heteroface solar cells used in space offer advantages of higher operating temperatures a...
The motivation for advanced solar cell flight experiments is discussed and the Advanced Solar Cell O...
Solar array design for any spacecraft is determined by the orbit parameters. For example, operationa...
A series of environmental tests were completed on one type of triple junction a-Si and two types of ...
The degradation of solar cells under irradiation by high energy particles (electrons, protons) is th...
An analysis of the effects of low energy proton irradiation on the electrical performance of triple ...
The vast majority of space probes to date have relied upon photovoltaic power generation. If future ...
NASA missions such as DAWN and JUNO, as well as the planned Europa Clipper mission, rely on solar po...
We investigated the effects of irradiation beam conditions on the performance degradation of silicon...
International audienceTo understand the influence of proton irradiation on lattice‐matched GaInP/GaA...
The Power Extension Package (PEP) is the prime focus of a development program to produce low cost so...
One of the major limitations of solar cells in space power systems is their vulnerability to radiati...
The results of an experimental evaluation of the real-time degradation characteristics of lithium-di...
The results of post-flight performance testing of the solar cells flown on the Advanced Photovoltaic...
Latest results of 3G28 triple-junction solar cells manufactured by AZUR SPACE Solar Power GmbH under...
GaAlAs/GaAs heteroface solar cells used in space offer advantages of higher operating temperatures a...
The motivation for advanced solar cell flight experiments is discussed and the Advanced Solar Cell O...
Solar array design for any spacecraft is determined by the orbit parameters. For example, operationa...