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Sunrise (telescope)

Sunrise Balloon-Borne Solar Observatory
Mission type Balloon-borne telescope
Operator Max Planck Institute for Solar System Research (MPS)
Website Official Page
Mission duration 6 days (2009), 5 days (2013)
Spacecraft properties
Manufacturer Max Planck Institute for Solar System Research
Kiepenheuer Institute for Solar Physics
High Altitude Observatory
Lockheed Martin Solar and Astrophysics Laboratory
Instituto de Astrofísica de Canarias
Instituto Nacional de Técnica Aeroespacial
Instituto de Astrofísica de Andalucía
Grupo de Astronomía y Ciencias del Espacio
Launch mass 2 t (2.0 long tons; 2.2 short tons)
Power 1.5 kW
Start of mission
Launch date 8 June 2009 and 12 June 2013
Rocket Balloon
Launch site Esrange Space Center
Kiruna, Sweden
End of mission
Landing date 14 June 2009 and 17 June 2013
Landing site Nunavut, Canada
Main
Wavelengths SuFI: 225, 280, 300, 313, 388 nm
IMaX: 525.06 nm
SUPOS: 854, 853.8 nm
Resolution 0.13-0.15 arcsec

The Sunrise balloon-borne solar observatory consists of a 1m aperture Gregory telescope, a UV filter imager, an imaging vector polarimeter, an image stabilization system and further infrastructure. The first science flight of Sunrise yielded high-quality data that reveal the structure, dynamics and evolution of solar convection, oscillations and magnetic fields at a resolution of around 100 km in the quiet Sun.

The strong absorption of UV radiation by the Earth's atmosphere makes it challenging to carry out ground-based observations at these wavelengths. A balloon mission reaching altitudes of above 30 km benefits from a reduction of UV absorption by 99%, making engineering solutions for the telescope easier. The launch site was in the arctic region to make uninterrupted observation of the Sun over several days possible. The telescope has a 1 metre primary mirror that directs the 1 kW of solar radiation to the first focal point where 99% of the radiation is reflected out of the telescope, the remaining light is transferred into several instruments.

The one metre diameter primary mirror is made from a glass ceramic zerodur, it is the central part of the gondola of nearly 2 tons. Solar panels of 1.5 kW output power are used to power the onboard equipment and a hard disk array of 2 x 2.4 Terabyte is used to store the data during flight.


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