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Demonstration and Design Criteria of Transition-Edge Sensors (TESs) with Noise Equivalent Power Below 10 (exp -19) W/Hz(sup 1/2) for Space-Borne Grating SpectrometersNo abstract available
Document ID
20150007345
Acquisition Source
Jet Propulsion Laboratory
Document Type
Presentation
External Source(s)
hdl:2014/44080
Authors
Beyer, A. D. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Kenyon, M. E. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Bumble, B. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Runyan, M. C. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Echternach, P. E. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Holmes, W. A. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Bock, J. J. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Bradford, C. M. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
May 5, 2015
Publication Date
June 24, 2013
Subject Category
Instrumentation And Photography
Meeting Information
Meeting: International Workshop on Low Temperature Detectors
Location: Pasadena, CA
Country: United States
Start Date: June 24, 2013
End Date: June 29, 2013
Sponsors: Jet Propulsion Lab., California Inst. of Tech.
Distribution Limits
Public
Copyright
Other
Keywords
transition-edge sensor (TES)
Background Limited Infrared Sub-mm Spectrograph (BLISS)

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