2014
DOI: 10.1117/12.2057321
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Performance characterization of UV science cameras developed for the Chromospheric Lyman-Alpha Spectro-Polarimeter (CLASP)

Abstract: The NASA Marshall Space Flight Center (MSFC) has developed a science camera suitable for sub-orbital missions for observations in the UV, EUV and soft X-ray. Six cameras will be built and tested for flight with the Chromospheric Lyman-Alpha Spectro-Polarimeter (CLASP), a joint National Astronomical Observatory of Japan (NAOJ) and MSFC sounding rocket mission. The goal of the CLASP mission is to observe the scattering polarization in Lyman-α and to detect the Hanle effect in the line core. Due to the nature of … Show more

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Cited by 8 publications
(6 citation statements)
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“…The MSFC developed CCD detector will detect the first-order diffraction. 4,5 The stigmatic optical design gives good performance on and off-axis, out to a 4 arcminute field angle. The desired performance across the full field is 6 arcsecond angular resolution, and ∼ 22 mÅ (7.5 -0.47 eV) spectral resolution.…”
Section: Magixs Instrumentmentioning
confidence: 99%
“…The MSFC developed CCD detector will detect the first-order diffraction. 4,5 The stigmatic optical design gives good performance on and off-axis, out to a 4 arcminute field angle. The desired performance across the full field is 6 arcsecond angular resolution, and ∼ 22 mÅ (7.5 -0.47 eV) spectral resolution.…”
Section: Magixs Instrumentmentioning
confidence: 99%
“…The equations to derive s phot and s CCD are the ones in Appendices A.1 and A.2 of Ishikawa et al (2014b). We employ an averaged read-out noise of sixelectrons (Champey et al 2014(Champey et al , 2015, which correspond to sixphotons. The averaged uncertainty is 0.066% at the Lyα core, 0.18% at the Lyα wing, and 0.50% at the Si III line.…”
Section: Scattering Polarization In the Si III Linementioning
confidence: 99%
“…The photon noise was calculated as the square root of the number of photoelectrons. The read-out noise was calculated based on the CCD calibration results of 6.2 and 6.5 e − rms per pixel for channel 1 and channel 2, respectively (Champey et al, 2014(Champey et al, , 2015. Variations of the signal larger than the noise can be seen in the wings, which indicate that the fluctuations from solar origin polarization might not be entirely cancelled out there.…”
Section: In-flight Polarization Calibrationmentioning
confidence: 99%