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Steven Christe 1 , S. Krucker 2 , L. Glesener 2 , S. Ishikawa 3 , B. Ramsey 4 , T. Takahashi 3 , R.P. Lin 2 1 NASA GSFC, Greenbelt, MD 2 Space Sciences Lab, UCB, Berkeley, CA 3 Dept. of Physics, U. of Tokyo, Japan 4 NASA MSFC, Huntsville, AL. The Focusing Optics X-ray Solar Imager (FOXSI). - PowerPoint PPT Presentation
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The Focusing Optics X-ray Solar Imager (FOXSI)Steven Christe1, S. Krucker2, L. Glesener2, S. Ishikawa3, B. Ramsey4, T. Takahashi3, R.P. Lin2
1 NASA GSFC, Greenbelt, MD2 Space Sciences Lab, UCB, Berkeley, CA3 Dept. of Physics, U. of Tokyo, Japan4 NASA MSFC, Huntsville, AL
Basic flare model.
Basic Flare ModelUpward beams
Accelerationsite
Downward beams
Chromospheric evaporation
HXR observations of flare-acceleration electrons Provide quantitative
measurements Depend on ambient
density Strongest from
footpoints Very faint emission from
corona RHESSI does not have
high enough sensitivity or dynamic range
HXR focusing optics can provide it.
HXR observations of Flare Model
Upward beams
Accelerationsite
Downward beams
Chromospheric evaporation
HXR
HXR
n = 109 cm-3
n = 1011 cm-3
n = 1011-12
cm-3
SXR
HXR observations of flare-acceleration electrons Provide quantitative
measurements Depend on ambient
density Strongest from
footpoints Very faint emission from
corona RHESSI does not have
high enough sensitivity or dynamic range
HXR focusing optics can provide it.
HXR observations of Flare Model
Upward beams
Accelerationsite
Downward beams
Chromospheric evaporation
HXR
HXR
n = 109 cm-3
n = 1011 cm-3
n = 1011-12
cm-3
SXR
HXR
HXR observations of flare-acceleration electrons Provide quantitative
measurements Depend on ambient
density Strongest from
footpoints Very faint emission from
corona RHESSI does not have
high enough sensitivity or dynamic range
HXR focusing optics can provide both
HXR observations of Flare Model
Upward beams
Accelerationsite
Downward beams
Chromospheric evaporation
HXR
HXR
n = 109 cm-3
n = 1011 cm-3
n = 1011-12
cm-3
SXR
HXR
Present day observations show mostly footpoints.
HXR observations of Flare Model
Upward beams
Accelerationsite
Downward beams
Chromospheric evaporation
n = 109 cm-3
n = 1011 cm-3
n = 1011-12
cm-3
SXR
RHESSI HXR Obs.
HXR
HXR
60 arcse
c
HXR focusing optics provides imaging of the acceleration region
And track electrons in the corona.
HXR observations of Flare Model
Upward beams
Accelerationsite
Downward beams
n = 109 cm-3
n = 1011-12
cm-3
SXR
HXR
HXR
Chromospheric evaporation
n = 1011 cm-3
HXRs from up and down beamsHX
R Fl
ux
Acceleration site
Height above the photosphere [arcsec]
ratio of footpoint to coronal emission depends on: coronal density electron spectrum photon energy trapping time
but it is generally large
Dynamic range: ~400
HXRs from up and down beamsHX
R Fl
ux
Height above the photosphere [arcsec]
?emission from acc. region?trapping?
Acceleration site Dynamic
range: ~400
ratio of footpoint to coronal emission depends on: coronal density electron spectrum photon energy trapping time
but it is generally large
Optics Performance
-100
-50 0 50
100
150arcsec
FWHM 10’’HPD 25’’
Point Spread Function (PSF)
Current Tech: slumped glass optics, replicated metal optics
Best resolution currently available by B. Ramsey (NASA MSFC)
Individual shell resolution: 7 arcsec (FWHM)
Telescope module resolution: 10-12 arcsec
Dynamic range: 30 arcsec:
~10050 arcsec:
~500
Metal optics-
1
0
-2-3-4-5
Log(
rela
tive
flux)
Dynamic range will allow us to image coronal HXR emission in the presence of HXR footpoints
Footpoints will be unresolved, but can be separated for larger flares
Basic Flare ModelUpward beams
Accelerationsite
Downward beams
n = 109
cm-3
n = 1011 cm-3
n = 1011-12
cm-3
SXR
5000
3000
1000
70025010020
90”
78”
66”
54”
42”
30”
18”6”
Dynamic Range
60 arcs
ec
HXR
HXR
HXRs from escaping electrons
Assuming 100 cm2
Dt=1 s
Dt=30 s
Assuming 100 cm2
2-4 kg/cm2 (e.g. 50 kg of optic = 100-200 cm2)
Jets
Quiet Sun network flares(coronal heating)
Active Region Flares
Radio bursts from shocks
Energetic Electrons
Type III radio bursts
CME
Position sensitive solid state (Si, CdTe, CZT) Energy resolution 0.2 to 2 keV (1-100 keV) Current Technology
Focal Plane Detectors
Type Pixels Pitch Range HeritageSi (strips) 128 x
12875 um 1-20 keV Astro-H HXI,
FOXSICdTe (strips) 128 x
128250 um 5-80 keV Astro-H HXI,
FOXSI2CZT 64 x 64 600 um 5-80 keV NuSTARCdTe 256 x
256250 um 2-80 keV HEXITEC
Parameter ValueFocal length 10 mEnergy Range 1-80 keVEnergy resolution ~1 keVSpatial resolution 7 arcsecDynamic Range Up to 100 x
RHESSISensitivity 100 x RHESSICost SMEX-like
FOXSI Mission ConceptThis mission concept is based on existing technology.
Currently FOXSI is a sounding rocket (launch Oct. ‘12). HEROES balloon launch in Sept ’13.
The future may bring better spatial resolution, lighter optics, etc.FOXSI will observe electrons as
they are being accelerated in the corona, along which field line they travel away from the acceleration site, where they are stopped, and how some electrons escape to be detected as SEPs at Earth.
Fin