dc.contributor.author | Noller, E. | en_US |
dc.date.accessioned | 2004-10-06 | |
dc.date.available | 2004-10-06 | |
dc.date.issued | 1994-07 | en_US |
dc.identifier.clearanceno | 94-0975 | en_US |
dc.identifier.uri | http://hdl.handle.net/2014/34620 | |
dc.description.abstract | Environmental testing and flight qualification of the TOPEX/POSEIDON spacecraft solar panels were performed with infrared (IR) lamps and a control system that were newly designed and integrated. The basic goal was more rigorous testing of the costly panels' new composite-structure design without jeopardizing their safety. The technique greatly reduces the costs and high risks of testing flight solar panels. | en_US |
dc.format.extent | 764704 bytes | |
dc.format.mimetype | application/pdf | |
dc.language.iso | en_US | |
dc.subject.other | environmental simulation solar panel thermal testing | en_US |
dc.title | The development of an Infrared Environmental System for TOPEX Solar Panel Testing | en_US |