{"@type": "dcat:Dataset", "accessLevel": "public", "bureauCode": ["026:00"], "contactPoint": {"@type": "vcard:Contact", "fn": "Samuel Krucker", "hasEmail": "mailto:krucker@ssl.berkeley.edu"}, "description": "&lt;p&gt;\r\n\tParticle acceleration in solar flares and its contribution to coronal heating are among the main&amp;nbsp; unsolved problems in heliophysics. Accelerated electrons in a plasma radiate hard X-ray (HXR)&amp;nbsp; emission through the well-known process of bremsstrahlung. HXR observations therefore are a&amp;nbsp; powerful diagnostic tool, providing quantitative measurements of flare-accelerated electrons. Since&amp;nbsp; bremsstrahlung emission depends on the density of the ambient medium, solar HXR emission is&amp;nbsp; usually brightest from below the transition region, where the density increases rapidly towards the&amp;nbsp; photosphere. Electron beams entering the chromosphere lose energy quickly through collisions and&amp;nbsp; produce relatively intense HXR emission at the footpoints of magnetic field lines. Electron beams&amp;nbsp; moving in the relatively tenuous corona suffer very few collisions, losing little energy and producing&amp;nbsp; only faint HXR emission. Present-day HXR instrumentation does not have the sensitivity to see&amp;nbsp; faint HXR emission from electrons traveling in the corona, nor the dynamic range to see such&amp;nbsp; faint emission in the presence of bright HXR footpoint emission in the chromosphere. Existing&amp;nbsp; observations therefore show us only where energetic electrons are stopped, but not where they&amp;nbsp; are accelerated, nor along what path they escape from the acceleration site. The most sensitive&amp;nbsp; solar HXR observations so far are provided by the Reuven Ramaty High Energy Spectroscopic&amp;nbsp; Imager (RHESSI) (Lin et al. 2002). These measurements are obtained with a non-focusing rotation&amp;nbsp; modulation collimator (RMC) imaging technique (Hurford et al. 2002). RMCs and other types&amp;nbsp; of non-focusing imaging, however, have intrinsically limited dynamic range and sensitivity. HXR&amp;nbsp; focusing optics can overcome both of these limitations (Section 1.2.2).&amp;nbsp;&lt;/p&gt;\r\n&lt;p&gt;\r\n\tThe Focusing Optics X-ray Solar Imager (FOXSI) is a sounding rocket payload funded under the&amp;nbsp; NASA Low Cost Access to Space (LCAS) program to test HXR focusing optics combined with&amp;nbsp; silicon strip detectors for solar observations (Krucker et al. 2009). The FOXSI program is being led&amp;nbsp; by the Space Sciences Laboratory at UC Berkeley in collaboration with the Marshall Space Flight&amp;nbsp; Center (MSFC) and the Japan Aerospace Exploration Agency (JAXA). FOXSI is on schedule&amp;nbsp; and on budget for a launch in October 2010. FOXSI will offer imaging spectroscopy and&amp;nbsp; unprecedented HXR sensitivity and dynamic range. FOXSI will be !100 times more sensitive than&amp;nbsp; RHESSI at 10 keV, and, for the first time, detect the non-thermal counterparts of quiet sun network&amp;nbsp; flares (Section 1.2.4).&amp;nbsp;&lt;/p&gt;\r\n&lt;p&gt;\r\n\tHere we propose a continuation of the FOXSI program which includes data analysis&amp;nbsp; and a second flight with an upgraded version of FOXSI. At moderate cost, we propose to&amp;nbsp; enhance the effective area, in particular at higher energies (by a factor of !4 at 15 keV), by adding&amp;nbsp; 3 more shells to the existing 7-shell optics (see Figure 9). Furthermore, our Japanese collaborators&amp;nbsp; will provide, at no cost, newly available double-sided cadmium telluride (CdTe) detectors as&amp;nbsp; a replacement for the Si detectors to allow us to take full advantage of the effective area at higher&amp;nbsp; energies. A second flight will therefore not only allow us to continue testing HXR focusing&amp;nbsp; optics for solar observations and also test newly developed CdTe strip detectors&amp;nbsp; in flight but is also expected to provide a significant increase in scientific return. In&amp;nbsp; this two year proposal, the first year (2011) will be used to upgrade the FOXSI payload and to&amp;nbsp; analyze data from the first flight, while the second flight is planned for the midd", "distribution": [{"@type": "dcat:Distribution", "downloadURL": "http://techport.nasa.gov/xml-api/10765", "format": "XML", "mediaType": "application/xml"}], "identifier": "TECHPORT_10765", "issued": "2010-11-01", "keyword": ["active", "project", "wallops-flight-facility"], "landingPage": "http://techport.nasa.gov/view/10765", "modified": "2025-03-31", "programCode": ["026:000"], "publisher": {"@type": "org:Organization", "name": "Science Mission Directorate"}, "references": ["http://techport.nasa.gov/doc/home/TechPort_Advanced_Search.pdf", "http://techport.nasa.gov/fetchFile?objectId=3447", "http://techport.nasa.gov/fetchFile?objectId=3448", "http://techport.nasa.gov/fetchFile?objectId=3456", "http://techport.nasa.gov/fetchFile?objectId=6560", "http://techport.nasa.gov/fetchFile?objectId=6561", "http://techport.nasa.gov/fetchFile?objectId=6584", "http://techport.nasa.gov/home"], "temporal": "2010-11-01T00:00:00Z/2013-10-01T00:00:00Z", "title": "The Focusing Optics X-ray Solar Imager (FOXSI): Update &amp; Second Launch Project"}