Zobrazeno 1 - 4
of 4
pro vyhledávání: '"Fawzy ElTohamy H. Amer"'
Publikováno v:
2022 13th International Conference on Electrical Engineering (ICEENG).
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ebabaf3180ebdace04173f99eb407f7e
https://doi.org/10.1109/iceeng49683.2022.9781878
https://doi.org/10.1109/iceeng49683.2022.9781878
Publikováno v:
Journal of Engineering Science and Military Technologies. 17:1-13
In this paper the reliability issue of a solar array of LEO spacecraft was analyzed with Failure Modes Effects and Criticality Analysis (FMECA) to ensure that the solar array will deliver the required power to the spacecraft until the end of life wit
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::1edd71600e4c7e663eb234d069615637
https://doi.org/10.21608/ejmtc.2017.21274
https://doi.org/10.21608/ejmtc.2017.21274
Publikováno v:
2018 IEEE Aerospace Conference.
The solar array is considered one of the famous and important primary power sources of a satellite. For solar array design, the required power and voltage level should be achieved to satisfy the requirements of the spacecraft Loads successfully. A ca
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::090817b8a44a16daed1f9b94050b07b0
https://doi.org/10.1109/aero.2018.8396384
https://doi.org/10.1109/aero.2018.8396384
Publikováno v:
2016 IEEE Aerospace Conference.
The spacecraft electrical power system design process is a very complex task; it depends on multiple issues, which will have a great effect on the trade-off analysis of designing Spacecraft Electrical Power System. It should also meet various design
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::fc2c5ba9892374fc9622d910cd173d7b
https://doi.org/10.1109/aero.2016.7500851
https://doi.org/10.1109/aero.2016.7500851