Bibcode
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.; Del Toro Iniesta, J. C.; López Jiménez, A.; Álvarez-Herrero, A.; Sabau-Graziati, L.; Widani, C.; Haberler, P.; Härtel, K.; Kampf, D.; Levin, T.; Pérez Grande, I.; Sanz-Andrés, A.; Schmidt, E.
Bibliographical reference
Solar Physics, Volume 268, Issue 1, pp.1-34
Advertised on:
1
2011
Journal
Citations
202
Refereed citations
181
Description
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.
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