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A Parametric Design Tool for Large Space Telescope SunshieldsIn what follows, we describe the thermal-mechanical model, the thermo-optical properties assumed for the components, and the environment which influences the thermal performance. Following this, we present predictions of performance sensitivity to variation in some of the optical characteristics. Studies of the performance sensitivity are continuing, to inform the direction of technology investment for further development of capabilities for large space telescopes.
Document ID
20080013266
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
External Source(s)
Authors
Paine, Christopher G.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Bradford, Charles M.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Dragovan, Mark C.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Yorke, Harold W.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 24, 2013
Publication Date
May 31, 2006
Subject Category
Space Sciences (General)
Meeting Information
Meeting: Astonomical Telescopes and Instrumentation Conference
Location: Orlando, Fl
Country: United States
Start Date: May 24, 2006
End Date: May 31, 2006
Distribution Limits
Public
Copyright
Other
Keywords
SAFIR
sunsheild
large space telescopes
V-groove radiator

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