Please use this identifier to cite or link to this item:
http://hdl.handle.net/11189/6322| DC Field | Value | Language |
|---|---|---|
| dc.contributor.author | Bayimissa, KDM | en_US |
| dc.contributor.author | Raji, Atanda K. | en_US |
| dc.contributor.author | Adonis, Marco Leroy | en_US |
| dc.date.accessioned | 2018-05-28T08:37:17Z | - |
| dc.date.available | 2018-05-28T08:37:17Z | - |
| dc.date.issued | 2016 | - |
| dc.identifier.uri | http://hdl.handle.net/11189/6322 | - |
| dc.description.abstract | The rapid development of modern technology has opened up the possibility to strive for an emerging class of a nanosatellite mission with a predictable lifespan, with one of the key factors determining the lifespan of a nanosatellite being the total radiation dose received by the spacecraft. | en_US |
| dc.language.iso | en | en_US |
| dc.publisher | ee publisher | en_US |
| dc.relation.ispartof | EngineerIT | en_US |
| dc.rights.uri | http://creativecommons.org/licenses/by-nc-sa/3.0/za/ | - |
| dc.subject | Radiation test | en_US |
| dc.subject | Nanosatellite | en_US |
| dc.subject | Spacecraft | en_US |
| dc.title | A radiation test on a front-end DC-DC power converter | en_US |
| dc.type.patent | Article | en_US |
| dc.identifier.doi | http://www.ee.co.za/article/radiation-test-front-end-dc-dc-power-converter.html | - |
| Appears in Collections: | Eng - Journal articles (DHET subsidised) | |
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