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The telescope and the double Fabry-Pérot interferometer for the ADAHELI solar space mission

Authors :
Greco, V
Cavallini, F
Berrilli, F
Velli, M
Roselli, L
Bigazzi, A
Moretti, Pf
Romoli, M
Orsini, S
Sabatini, P
Carbone, V
Consolini, G
Di Mauro MP
Ermolli, I
Pietropaolo, Ermanno
Romano, P
Ventura, P
Valdettaro, L
White, Sm
Zuccarello, F
Cauzzi, G
Giammaria, F
Reardon, K
Briguglio, R
Landi, S
Vecchio, A
Lepreti, F
Sorriso Valvo, L
Contarino, L
Guglielmino, S
De Pontieu, B
Cardini, D
Chieffi, A
Milillo, A
Mura, A
De Angelis, E
Mangano, V
Selci, S
Criscuoli, S
Giorgi, F
Alimenti, F
Palazzari, V
Biferale, L
Cantarano, S
Del Moro, D
Egidi, A
Penza, V
Piazzesi, R
Stangalini, M
Vantaggiato, M
Viticchiè, B
Casolino, M
De Santis, C
Sparvoli, R.
Source :
Conference on Space Telescopes and Instrumentation 2010-Optical, Infrared, and Millimeter Wave, San Diego, June 27-JUL 02, 2010, pp. 773142–773142, San Diego, 2010, info:cnr-pdr/source/autori:Greco, Vincenzo (a); Cavallini, F. (b), Berrilli F. (c)/congresso_nome:Conference on Space Telescopes and Instrumentation 2010-Optical, Infrared, and Millimeter Wave, San Diego, June 27-JUL 02, 2010/congresso_luogo:San Diego/congresso_data:2010/anno:2010/pagina_da:773142/pagina_a:773142/intervallo_pagine:773142–773142
Publication Year :
2010
Publisher :
SPIE, 2010.

Abstract

ADvanced Astronomy for HELIophysics (ADAHELI) is a Small Mission to study the structure and fast dynamics of the low solar atmosphere, performing Visible-NIR monochromatic and broad-band observations. The mission will achieve millimeter full disk observations as well. The ADAHELI Team has succesfully completed, in December 2008, the Phase A study awarded by the Italian Space Agency (ASI). The Interferometer for SOlar Dynamics (ISODY), on board the ADAHELI satellite, comprises a Gregorian telescope and its focal plane suite. The advanced design focal plane suite uses fast CMOS cameras for investigating photospheric and chromospheric fast dynamics and structure. ISODY is equipped with a pioneering focal plane suite composed of a spectral channel, based upon a tandem of Fabry-Perot interferometers operating in the visible-NIR spectral region, a broad band channel for high resolution imaging, and a correlation tracker used as an image stabilization system. ADAHELI's mission profile has been tailored to limit the spacecraft's radial velocity in the Sunward direction, to not exceed ±4 km/s, during 95% of the yearly orbit, to allow a continuous use of the on-board interferometer.

Details

ISSN :
0277786X
Database :
OpenAIRE
Journal :
SPIE Proceedings
Accession number :
edsair.doi.dedup.....571b8bb0f3d11f0b3381ff79ea44f022