Paper
26 September 2013 OSIRIS-REx OCAMS detector assembly characterization
J. Hancock, B. Crowther, M. Whiteley, R. Burt, M. Watson, J. Nelson, C. Fellows, B. Rizk, E. Kinney-Spano, M. Perry, M. Hunten
Author Affiliations +
Abstract
The OSIRIS-REx asteroid sample return mission carries a suite of three cameras referred to as OCAMS. The Space Dynamics Laboratory (SDL) at Utah State University is providing the CCD-based detector assemblies for OCAMS to the Lunar Planetary Lab (LPL) at the University of Arizona. Working with the LPL, SDL has designed the electronics to operate a 1K by 1K frame transfer Teledyne DALSA Multi-Pinned Phase (MPP) CCD. The detector assembly electronics provides the CCD clocking, biasing, and digital interface with the OCAMS payload Command Control Module (CCM). A prototype system was built to verify the functionality of the detector assembly design and to characterize the detector system performance at the intended operating temperatures. The characterization results are described in this paper.
© (2013) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
J. Hancock, B. Crowther, M. Whiteley, R. Burt, M. Watson, J. Nelson, C. Fellows, B. Rizk, E. Kinney-Spano, M. Perry, and M. Hunten "OSIRIS-REx OCAMS detector assembly characterization", Proc. SPIE 8860, UV/Optical/IR Space Telescopes and Instruments: Innovative Technologies and Concepts VI, 88600J (26 September 2013); https://doi.org/10.1117/12.2024665
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Cited by 2 scholarly publications.
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KEYWORDS
Sensors

Charge-coupled devices

Cameras

CCD image sensors

Electronics

Light emitting diodes

Interfaces

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