| Presentation | 1998/1/30 Consideration in System Design to Increase Robustness to Component Failure Masanori Homma, |
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| PDF Download Page | PDF download Page Link |
| Abstract(in Japanese) | (See Japanese page) |
| Abstract(in English) | In system design of satellite, high reliability is required as well as high performance. Mechanical components are usually "the single point" from its nature. So it is very important to design the satellite system in consideration with the case that failure would occur at those components. This paper describes some examples in ETS-8 to avoid fatal trouble in failure of the large deployable antenna or apogee engine. |
| Keyword(in Japanese) | (See Japanese page) |
| Keyword(in English) | ETS-8 / component failure / single point / system design |
| Paper # | SANE97-121 |
| Date of Issue |
| Conference Information | |
| Committee | SANE |
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| Conference Date | 1998/1/30(1days) |
| Place (in Japanese) | (See Japanese page) |
| Place (in English) | |
| Topics (in Japanese) | (See Japanese page) |
| Topics (in English) | |
| Chair | |
| Vice Chair | |
| Secretary | |
| Assistant | |
| Paper Information | |
| Registration To | Space, Aeronautical and Navigational Electronics (SANE) |
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| Language | JPN |
| Title (in Japanese) | (See Japanese page) |
| Sub Title (in Japanese) | (See Japanese page) |
| Title (in English) | Consideration in System Design to Increase Robustness to Component Failure |
| Sub Title (in English) | |
| Keyword(1) | ETS-8 |
| Keyword(2) | component failure |
| Keyword(3) | single point |
| Keyword(4) | system design |
| 1st Author's Name | Masanori Homma |
| 1st Author's Affiliation | National Space Development Agency of Japan() |
| Date | 1998/1/30 |
| Paper # | SANE97-121 |
| Volume (vol) | vol.97 |
| Number (no) | 523 |
| Page | pp.pp.- |
| #Pages | 4 |
| Date of Issue | |