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James Webb Space Telescope: Large Deployable Cryogenic Telescope in SpaceThe James Webb Space Telescope (JWST) is an infrared space telescope designed to explore four major science themes: first light and reionization, the assembly of galaxies, the birth of stars and protoplanetary systems, and planetary systems and origins of life. JWST is a segmented architecture telescope with an aperture of 6.6 m. It will operate at cryogenic temperature (40 K), achieved via passive cooling, in an orbit about the Earth-Sun second Lagrange point (L2). Passive cooling is facilitated by means of a large sunshield that provides thermal isolation and protection from direct illumination from the Sun. The large size of the telescope and spacecraft systems require that they are stowed for launch in a configuration that fits the Ariane 5 fairing, and then deployed after launch. Routine wavefront sensing and control measurements are used to achieve phasing of the segmented primary mirror and initial alignment of the telescope. A suite of instruments will provide the capability to observe over a spectral range from 0.6- to 27-micron wavelengths with imaging and spectroscopic configurations. An overview is presented of the architecture and selected optical design features of JWST are described
Document ID
20120016025
Acquisition Source
Goddard Space Flight Center
Document Type
Reprint (Version printed in journal)
Authors
Lightsey, Paul A.
(Ball Aerospace and Technologies Corp. Boulder, CO, United States)
Atkinson, Charles
(Northrop Grumman Aerospace Systems Redondo Beach, CA, United States)
Clampin, Mark
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Feinberg, Lee D.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
August 26, 2013
Publication Date
January 1, 2012
Publication Information
Publication: Optical Engineering
Volume: 51
Issue: 1
Subject Category
Astronomy
Report/Patent Number
GSFC.JA.7276.2012
Funding Number(s)
CONTRACT_GRANT: NAS5-02200
Distribution Limits
Public
Copyright
Other

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