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Development and Testing of an Innovative Two-Arm Focal-Plane Thermal Strap (TAFTS)Maintaining temperature stability in optical focal planes comes with the intrinsic challenge of creating a pathway that is both extremely flexible mechanically and highly conductive thermally. The task is further complicated because science‐caliber optical focal planes are extremely delicate, yet their mechanical resiliency is rarely tested and documented. The mechanical engineer tasked with the thermo‐mechanical design must then create a highly conductive thermal link that minimizes the tensile and shear stresses transmitted to the focal plane without design parameters on an acceptable stiffness. This paper will describe the development and testing of the thermal link developed for the Portable Remote Imaging Spectrometer (PRISM) instrument. It will provide experimentally determined mechanical stiffness plots in the three axes of interest. Analytical and experimental thermal conductance results for the two‐arm focal‐plane thermal strap (TAFTS), from cryogenic to room temperatures, are also presented. The paper also briefly describes some elements of the fabrication process followed in developing a novel design solution, which provides high conductance and symmetrical mechanical loading, while providing enhanced flexibility in all three degrees of freedom.
Document ID
20150006987
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
External Source(s)
Authors
Urquiza, E.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Vasquez, C.
(California Polytechnic State Univ. San Luis Obispo, CA, United States)
Rodriguez, J.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Van Gorp, B.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
April 30, 2015
Publication Date
June 8, 2011
Subject Category
Mechanical Engineering
Meeting Information
Meeting: Space Cryogenics Workshop (SCW)
Location: Coeur dýAlene, ID
Country: United States
Start Date: June 8, 2011
End Date: June 10, 2011
Sponsors: NASA Headquarters
Distribution Limits
Public
Copyright
Other
Keywords
flexible thermal strap
conduction cooling

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