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The Origins Space Telescope Cryo-Thermal ArchitectureThe Origins Space Telescope (OST) is studied as a future Mid- and Far-Infrared flagship-class observatory. OST will cover the wavelength range from 6 to 600 microns. To reach the sky background for 200-micron wavelengths temperatures of 4 degrees Kelvin or lower are required. To achieve this low temperature active cooling is required, along with passive shielding and passive radiation to deep space. Currently two concepts are being studied: Concept 1 with a 9-meter-diameter primary and a suite of 5 extremely capable instruments providing both imaging and spectroscopy over the entire wavelength range. Concept 2 is a more modest sized telescope with a collecting area equivalent to a 5-meter primary, fewer deployments and 3 or 4 instruments also covering the entire wavelength range for imaging and spectroscopy, although with somewhat reduced spectroscopic resolution, and somewhat slower mapping speed. This paper will describe OST Concept 2's cryogenic thermal architecture and thermal model results.
Document ID
20180004070
Acquisition Source
Goddard Space Flight Center
Document Type
Presentation
Authors
DiPirro, M.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Fantano, L.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
July 31, 2018
Publication Date
June 10, 2018
Subject Category
Astronomy
Report/Patent Number
GSFC-E-DAA-TN57412
Meeting Information
Meeting: SPIE Astronomical Telescopes + Instrumentation 2018
Location: Austin, TX
Country: United States
Start Date: June 10, 2018
End Date: June 15, 2018
Sponsors: International Society for Optical Engineering
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
Space Telescope
cryogenics
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