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Vibrations loads in the process of designing scientific spacecraft payloads
Citation
Gómez San Juan, Alejandro Manuel and Navarro Medina, Fermín and Cubas Cano, Javier and Sorribes Palmer, Felix and Fernandez Rico, German and Alonso, Gustavo (2013). Vibrations loads in the process of designing scientific spacecraft payloads. In: "11th International Conference on Vibration Problems", 09/09/2013 - 12/09/2013, Lisboa (Portugal). pp. 1-11.
Description
| Title: | Vibrations loads in the process of designing scientific spacecraft payloads |
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| Author/s: |
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| Item Type: | Presentation at Congress or Conference (Article) |
| Event Title: | 11th International Conference on Vibration Problems |
| Event Dates: | 09/09/2013 - 12/09/2013 |
| Event Location: | Lisboa (Portugal) |
| Title of Book: | ICOVP-2013 |
| Date: | 9 September 2013 |
| Subjects: | |
| Freetext Keywords: | Spacecraft, Random, Acoustic, Sine, FEM, SEA |
| Faculty: | E.T.S.I. Aeronáuticos (UPM) |
| Department: | Otro |
| Creative Commons Licenses: | Recognition - No derivative works - Non commercial |
Abstract
Scientific missions constitute fundamental cornerstones of space agencies such as ESA and NASA. Modern astronomy could not be understood without the data provided by these missions. Scientists need to design very carefully onboard instruments. Payloads have to survive the crucial launch moment and later perform well in the really harsh space environ-ment. It is very important that the instrument conceptual idea can be engineered to sustain all those loads
More information
| Item ID: | 26140 |
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| DC Identifier: | https://oa.upm.es/26140/ |
| OAI Identifier: | oai:oa.upm.es:26140 |
| Official URL: | http://www.icovp.com/components/com_breezingforms/exports/625_0.pdf |
| Deposited by: | Memoria Investigacion |
| Deposited on: | 12 Jun 2014 18:20 |
| Last Modified: | 14 Nov 2014 09:58 |
