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Induced shock loads during the separation of the Ariane 5 VEB structure
Cita
Huerta Gómez de Merodio, María Consuelo 
ORCID: https://orcid.org/0000-0001-8521-3512, Gómez-Molinero, V., Alarcón Álvarez, Enrique ORCID: https://orcid.org/0000-0001-6538-7814, Gómez Lera, Sagrario ORCID: https://orcid.org/0000-0002-0715-5051 and Molina Ruiz, Francisco Javier
(1989).
Induced shock loads during the separation of the Ariane 5 VEB structure.
En: "International Conference on Spacecraft Structures and Mechanical Testing", 19/10/1989-21/10/1989, Noordwijk, The Netherlands.
ORCID: https://orcid.org/0000-0001-8521-3512, Gómez-Molinero, V., Alarcón Álvarez, Enrique ORCID: https://orcid.org/0000-0001-6538-7814, Gómez Lera, Sagrario ORCID: https://orcid.org/0000-0002-0715-5051 and Molina Ruiz, Francisco Javier
(1989).
Induced shock loads during the separation of the Ariane 5 VEB structure.
En: "International Conference on Spacecraft Structures and Mechanical Testing", 19/10/1989-21/10/1989, Noordwijk, The Netherlands.
Descripción
| Título: | Induced shock loads during the separation of the Ariane 5 VEB structure |
|---|---|
| Autor/es: |
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| Tipo de Documento: | Ponencia en Congreso o Jornada (Artículo) |
| Título del Evento: | International Conference on Spacecraft Structures and Mechanical Testing |
| Fechas del Evento: | 19/10/1989-21/10/1989 |
| Lugar del Evento: | Noordwijk, The Netherlands |
| Título del Libro: | Spacecraft Structures and Mechanical Testing : proceedings of the international conference |
| Fecha: | 1989 |
| Materias: | |
| ODS: | |
| Palabras Clave Informales: | Ariane launch vehicle ; Dynamic structural analysis ; Mathematical models ; Shock loads ; Systems simulation, Finite element method ; Performance prediction ; Performance tests ; Wave propagation |
| Escuela: | E.T.S.I. Industriales (UPM) |
| Departamento: | Mecánica Estructural y Construcciones Industriales [hasta 2014] |
| Licencias Creative Commons: | Reconocimiento - Sin obra derivada - No comercial |
Resumen
Tests used to simulate the separation of the lower stage of the Ariane Vehicle Equipment Bay (VEB) were carried out on a flat full scale model. Theoretical studies carried out prior to testing are described. Three different mathematical methods, finite element, component element, and wave propagation, were used. Comparison of the predicted theoretical results with the actual test results is planned.
Más información
| ID de Registro: | 20827 |
|---|---|
| Identificador DC: | https://oa.upm.es/20827/ |
| Identificador OAI: | oai:oa.upm.es:20827 |
| URL Oficial: | http://www.esa.int/About_Us/ESA_Publications |
| Depositado por: | Biblioteca ETSI Industriales |
| Depositado el: | 30 Sep 2013 09:00 |
| Ultima Modificación: | 26 May 2017 15:27 |
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