Problems of irradiance characteristics measurement of solar simulators for ground spacecraft tests
The reliability of both spacecraft as a whole and of their systems is confirmed at the stage of complex ground-based experimental tests, including complex thermal vacuum tests. The thermal state of the test object in thermal vacuum chambers is obtaining, in particular, using a solar simulator. Radio...
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Association «Technology Platform «National Information Satellite System»
2020-10-01
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doaj-c2707a7d36b547d0a08640ca68cc10dc2020-11-25T03:46:43ZrusAssociation «Technology Platform «National Information Satellite System»Космические аппараты и технологии2618-79572020-10-014312914010.26732/j.st.2020.3.01Problems of irradiance characteristics measurement of solar simulators for ground spacecraft testsA. A. Shevchuk0O. V. Pastushenko1V. V. Dvirniy2G. V. Dvirniy3A. A. Filatov4JSC «Academician M. F. Reshetnev» Information Satellite Systems»JSC «Academician M. F. Reshetnev» Information Satellite Systems»Siberian Federal UniversityReshetnev Siberian State University of Science and TechnologyLLC NPO HeliosferaThe reliability of both spacecraft as a whole and of their systems is confirmed at the stage of complex ground-based experimental tests, including complex thermal vacuum tests. The thermal state of the test object in thermal vacuum chambers is obtaining, in particular, using a solar simulator. Radiometers based on silicon photoelectric converters are most often used to control the irradiance of a solar simulator under conditions of thermal vacuum tests. At the same time, an analysis of the features of silicon photoelectric converters shows that their direct measurement with the accuracy required for ground-based tests of spacecraft is impossible; their output is nonlinear, depends on the received spectrum, their own temperature and has long-term instability. The achieved measurement accuracy directly depends on the number and accuracy of the tools used and the methods of the necessary correction, of which the mismatch correction between the solar simulator spectrum and the solar spectrum is the most difficult and laborious. At the same time, spectrally nonselective heat flux radiometers are free from the above disadvantages. In the course of the experiment we carried out, the significant dependence of the accuracy of measuring the irradiance with radiometers based on silicon photoelectric converters on the received spectrum was confirmed. The conclusion is made that direct measurement by heat flux radiometers of the irradiance of the solar simulator is most justified under the conditions of thermal vacuum tests.http://journal-niss.ru/en/archive_view.php?num=227thermal vacuum testssolar simulatorirradiancespectral mismatchphotoelectric converterheat flux radiometer |
collection |
DOAJ |
language |
Russian |
format |
Article |
sources |
DOAJ |
author |
A. A. Shevchuk O. V. Pastushenko V. V. Dvirniy G. V. Dvirniy A. A. Filatov |
spellingShingle |
A. A. Shevchuk O. V. Pastushenko V. V. Dvirniy G. V. Dvirniy A. A. Filatov Problems of irradiance characteristics measurement of solar simulators for ground spacecraft tests Космические аппараты и технологии thermal vacuum tests solar simulator irradiance spectral mismatch photoelectric converter heat flux radiometer |
author_facet |
A. A. Shevchuk O. V. Pastushenko V. V. Dvirniy G. V. Dvirniy A. A. Filatov |
author_sort |
A. A. Shevchuk |
title |
Problems of irradiance characteristics measurement of solar simulators for ground spacecraft tests |
title_short |
Problems of irradiance characteristics measurement of solar simulators for ground spacecraft tests |
title_full |
Problems of irradiance characteristics measurement of solar simulators for ground spacecraft tests |
title_fullStr |
Problems of irradiance characteristics measurement of solar simulators for ground spacecraft tests |
title_full_unstemmed |
Problems of irradiance characteristics measurement of solar simulators for ground spacecraft tests |
title_sort |
problems of irradiance characteristics measurement of solar simulators for ground spacecraft tests |
publisher |
Association «Technology Platform «National Information Satellite System» |
series |
Космические аппараты и технологии |
issn |
2618-7957 |
publishDate |
2020-10-01 |
description |
The reliability of both spacecraft as a whole and of their systems is confirmed at the stage of complex ground-based experimental tests, including complex thermal vacuum tests. The thermal state of the test object in thermal vacuum chambers is obtaining, in particular, using a solar simulator. Radiometers based on silicon photoelectric converters are most often used to control the irradiance of a solar simulator under conditions of thermal vacuum tests. At the same time, an analysis of the features of silicon photoelectric converters shows that their direct measurement with the accuracy required for ground-based tests of spacecraft is impossible; their output is nonlinear, depends on the received spectrum, their own temperature and has long-term instability. The achieved measurement accuracy directly depends on the number and accuracy of the tools used and the methods of the necessary correction, of which the mismatch correction between the solar simulator spectrum and the solar spectrum is the most difficult and laborious. At the same time, spectrally nonselective heat flux radiometers are free from the above disadvantages. In the course of the experiment we carried out, the significant dependence of the accuracy of measuring the irradiance with radiometers based on silicon photoelectric converters on the received spectrum was confirmed. The conclusion is made that direct measurement by heat flux radiometers of the irradiance of the solar simulator is most justified under the conditions of thermal vacuum tests. |
topic |
thermal vacuum tests solar simulator irradiance spectral mismatch photoelectric converter heat flux radiometer |
url |
http://journal-niss.ru/en/archive_view.php?num=227 |
work_keys_str_mv |
AT aashevchuk problemsofirradiancecharacteristicsmeasurementofsolarsimulatorsforgroundspacecrafttests AT ovpastushenko problemsofirradiancecharacteristicsmeasurementofsolarsimulatorsforgroundspacecrafttests AT vvdvirniy problemsofirradiancecharacteristicsmeasurementofsolarsimulatorsforgroundspacecrafttests AT gvdvirniy problemsofirradiancecharacteristicsmeasurementofsolarsimulatorsforgroundspacecrafttests AT aafilatov problemsofirradiancecharacteristicsmeasurementofsolarsimulatorsforgroundspacecrafttests |
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