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Continued Development of a Precision Cryogenic Dilatometer for the James Webb Space TelescopeAs part of the James Webb Space Telescope (JWST) materials working group, a novel cryogenic dilatometer was designed and built at NASA Jet Propulsion Laboratory to help address stringent coefficient of thermal expansion (CTE) knowledge requirements. Previously reported results and error analysis have estimated a CTE measurement accuracy for ULE of 1.7 ppb/K with a 20K thermal load and 0.1 ppb/K with a 280K thermal load. Presented here is a further discussion of the cryogenic dilatometer system and a description of recent work including system modifications and investigations.
Document ID
20100009706
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
External Source(s)
Authors
Karlmann, Paul B.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Dudik, Matthew J.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Halverson, Peter G.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Levine, Marie
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Marcin, Martin
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Peters, Robert D.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Shaklan, Stuart
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
VanBuren, David
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 25, 2013
Publication Date
August 24, 2004
Subject Category
Mechanical Engineering
Meeting Information
Meeting: SPIE 49th Annual Meeting
Location: Denver, CO
Country: United States
Start Date: August 2, 2004
End Date: August 6, 2004
Sponsors: International Society for Optical Engineering
Distribution Limits
Public
Copyright
Other
Keywords
thermal strain
dilatometer
coefficient of thermal expansion
fused silica
zerodur

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