Solar-B
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Mullard Space Science Laboratory
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About Solar-B
Solar-B is due for launch in 2005 on an ISAS (Institute of Space and
Astronautical Science) M V rocket. It will be placed in a polar sun-synchronous
orbit with an inclination of 97.9 degrees. The nominal mission lifetime is 3
years.
The instrument payload consists of:
Solar Optical
Telescope (SOT)
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This will be the first large optical telescope flown in space. Its
aperture is 50cm and angular resolution achieved will be 0.25" (175km on the
Sun) covering a wavelength range of 480-650nm.
SOT also includes the Focal Plane Package (FPP) vector magnetograph and
spectrograph. The vector magnetograph will provide time series of photospheric
vector magnetograms, Doppler velocity and photospheric intensity.
Magnetic lines: Fe I 525.0nm, Fe I 630.2nm, Continuum:524.6nm,
Velocity: Fe I 532.4nm
FOV: 164x164"
Magnetic sensitivity: B(longitudinal): 1-5G, B(transverse): 30-50G
Temporal resolution: 5 mins
The FPP spectrograph has a spectral resolution of 2.0nm and provides detailed
Stokes line profiles of intensity and polarization.
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X-ray Telescope (XRT)
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XRT will provide coronal images at different temperatures, both full disk and
partial fields of view.
Temperature range: 6.1 < log T < 7.5
Temperature discrimination: log T=0.2
Angular resolution: 2"
Temporal resolution: cadence=2s (reduced FOV), exposure time: min=4ms, max=10s
FOV: Full disk (>30 arc min)
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EUV Imaging Spectrometer (EIS)
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The telescope is an off-axis paraboloid design, with focal length 1.9m and
mirror diameter 150mm. EIS has a total length of 3m. Multilayer toroidal gratings disperse the spectrum
onto 2 detectors covering 40A each.
Wavelength range: 170-210A
240-290 A
Angular resolution: 2". Four slit/slot positions are available -
1" slit, 2" slit, 40" slot and 240" have been determined.
Spectral/Velocity resolution: 3km/s for Doppler velocities, 20km/s for line
widths
Temporal resolution:
  In sectrosocopy mode: < 1s in dynamic events
~ 10s in active regions
  In imaging mode: monochromatic imaging of an active
region (~4x4 arc min) in 3s for dynamic
events, 10s otherwise.
FOV: 360"x512"
EIS will provide monochromatic images of the transition region and corona
at high cadence using a slot. High spectral resolution images can be obtained
by rastering with a slit.
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