NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Due to the lapse in federal government funding, NASA is not updating this website. We sincerely regret this inconvenience.

Back to Results
Performance Characterization of UV Science Cameras Developed for the Chromospheric Lyman-Alpha Spectro-PolarimeterThe 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-alpha and to detect the Hanle effect in the line core. Due to the nature of Lyman-alpha polarization in the chromosphere, strict measurement sensitivity requirements are imposed on the CLASP polarimeter and spectrograph systems; science requirements for polarization measurements of Q/I and U/I are 0.1 percent in the line core. CLASP is a dual-beam spectro- polarimeter, which uses a continuously rotating waveplate as a polarization modulator, while the waveplate motor driver outputs trigger pulses to synchronize the exposures. The CCDs are operated in frame-transfer mode; the trigger pulse initiates the frame transfer, effectively ending the ongoing exposure and starting the next. The strict requirement of 0.1 percent polarization accuracy is met by using frame-transfer cameras to maximize the duty cycle in order to minimize photon noise. Coating the e2v CCD57-10 512x512 detectors with Lumogen-E coating allows for a relatively high (30 percent) quantum efficiency at the Lyman-alpha line. The CLASP cameras were designed to operate with a gain of 2.0 +/- 0.5, less than or equal to 25 e- readout noise, less than or equal to 10 e-/second/pixel dark current, and less than 0.1percent residual non-linearity. We present the results of the performance characterization study performed on the CLASP prototype camera; system gain, dark current, read noise, and residual non-linearity.
Document ID
20140011800
Acquisition Source
Marshall Space Flight Center
Document Type
Abstract
Authors
Champey, Patrick
(Alabama Univ. Huntsville, AL, United States)
Kobayashi, Ken
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Winebarger, Amy
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Cirtain, Jonathan
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Hyde, David
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Robertson, Bryan
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Beabout, Brent
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Beabout, Dyana
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Stewart, Mike
(Alabama Univ. Huntsville, AL, United States)
Date Acquired
September 17, 2014
Publication Date
June 13, 2014
Subject Category
Instrumentation And Photography
Report/Patent Number
M14-3797
Report Number: M14-3797
Meeting Information
Meeting: SPIE Astronomical Telescopes and Instrumentation 2014
Location: Montreal, Quebec
Country: Canada
Start Date: June 22, 2014
End Date: June 27, 2014
Sponsors: International Society for Optical Engineering
Distribution Limits
Public
Copyright
Public Use Permitted.
No Preview Available