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Barthol, P., Gandorfer, A., Solanki, S. K., Schüssler, M., Chares, B., Curdt, W., Deutsch, W., Feller, A., Germerott, D., Grauf, B., Heerlein, K., Hirzberger, J., Kolleck, M., Meller, R., Müller, R., Riethmüller, T. L., Tomasch, G., Knölker, M., Lites, B. W., Card, G., Elmore, D., Fox, J., Lecinski, A., Nelson, P., Summers, R., Watt, A., Martínez Pillet, V., Bonet, J. A., Schmidt, W., Berkefeld, T., Title, A. M., Domingo, V., Gasent Blesa, J. L., Toro Iniesta, J. C. del, López Jiménez, A., Álvarez Herrero, A., Sabau Graziati, L., Widani, C., Haberler, P., Härtel, K., Kampf, D., Levin, T., Pérez Grande, María Isabel ORCID: https://orcid.org/0000-0002-7145-2835, Sanz Andres, Angel Pedro ORCID: https://orcid.org/0000-0001-5890-6065 and Schmidt, E. (2010). The Sunrise Mission. "Solar Physics", v. 268 (n. 1); pp. 1-34. ISSN 0038-0938. https://doi.org/10.1007/s11207-010-9662-9.
Título: | The Sunrise Mission |
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Autor/es: |
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Tipo de Documento: | Artículo |
Título de Revista/Publicación: | Solar Physics |
Fecha: | Noviembre 2010 |
ISSN: | 0038-0938 |
Volumen: | 268 |
Materias: | |
Palabras Clave Informales: | Instrumentation and data management, Integrated sun observations, Magnetic fields, photosphere |
Escuela: | E.T.S.I. Aeronáuticos (UPM) [antigua denominación] |
Departamento: | Motopropulsión y Termofluidodinámica [hasta 2014] |
Licencias Creative Commons: | Reconocimiento - Sin obra derivada - No comercial |
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The first science flight of the balloon-borne Sunrise telescope took place in June 2009 from ESRANGE (near Kiruna/Sweden) to Somerset Island in northern Canada. We describe the scientific aims and mission concept of the project and give an overview and a description of the various hardware components: the 1-m main telescope with its postfocus science instruments (the UV filter imager SuFI and the imaging vector magnetograph IMaX) and support instruments (image stabilizing and light distribution system ISLiD and correlating wavefront sensor CWS), the optomechanical support structure and the instrument mounting concept, the gondola structure and the power, pointing, and telemetry systems, and the general electronics architecture. We also explain the optimization of the structural and thermal design of the complete payload. The preparations for the science flight are described, including AIV and ground calibration of the instruments. The course of events during the science flight is outlined, up to the recovery activities. Finally, the in-flight performance of the instrumentation is discussed.
ID de Registro: | 6971 |
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Identificador DC: | https://oa.upm.es/6971/ |
Identificador OAI: | oai:oa.upm.es:6971 |
Identificador DOI: | 10.1007/s11207-010-9662-9 |
URL Oficial: | http://www.springerlink.com/content/0038-0938/ |
Depositado por: | Memoria Investigacion |
Depositado el: | 31 May 2011 08:22 |
Ultima Modificación: | 20 Abr 2016 16:05 |