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A Future Large-Aperture UVOIR Space Observatory: Key Technologies and CapabilitiesWe present the key technologies and capabilities that will enable a future, large-aperture ultravioletopticalinfrared (UVOIR) space observatory. These include starlight suppression systems, vibration isolation and control systems, lightweight mirror segments, detector systems, and mirror coatings. These capabilities will provide major advances over current and near-future observatories for sensitivity, angular resolution, and starlight suppression. The goals adopted in our study for the starlight suppression system are 10-10 contrast with an inner working angle of 20 milliarcsec and broad bandpass. We estimate that a vibration and isolation control system that achieves a total system vibration isolation of 140 dB for a vibration-isolated mass of 5000 kg is required to achieve the high wavefront error stability needed for exoplanet coronagraphy. Technology challenges for lightweight mirror segments include diffraction-limited optical quality and high wavefront error stability as well as low cost, low mass, and rapid fabrication. Key challenges for the detector systems include visible-blind, high quantum efficiency UV arrays, photon counting visible and NIR arrays for coronagraphic spectroscopy and starlight wavefront sensing and control, and detectors with deep full wells with low persistence and radiation tolerance to enable transit imaging and spectroscopy at all wavelengths. Finally, mirror coatings with high reflectivity ( 90), high uniformity ( 1) and low polarization ( 1) that are scalable to large diameter mirror substrates will be essential for ensuring that both high throughput UV observations and high contrast observations can be performed by the same observatory.
Document ID
20150000801
Acquisition Source
Goddard Space Flight Center
Document Type
Presentation
Authors
Bolcar, Matthew Ryan
(NASA Goddard Space Flight Center Greenbelt, MD United States)
Stahle, Carl M.
(NASA Goddard Space Flight Center Greenbelt, MD United States)
Balasubramaniam, Kunjithapatham
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, 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)
Mosier, Gary E.
(NASA Goddard Space Flight Center Greenbelt, MD United States)
Quijada, Manuel A.
(NASA Goddard Space Flight Center Greenbelt, MD United States)
Rauscher, Bernard J.
(NASA Goddard Space Flight Center Greenbelt, MD United States)
Redding, David C.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Rioux, Norman M.
(NASA Goddard Space Flight Center Greenbelt, MD United States)
Shaklan, Stuart B.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Stahl, H. Philip
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Thronson, Harley A.
(NASA Goddard Space Flight Center Greenbelt, MD United States)
Date Acquired
January 26, 2015
Publication Date
January 4, 2015
Subject Category
Optics
Astronomy
Report/Patent Number
GSFC-E-DAA-TN19939
Report Number: GSFC-E-DAA-TN19939
Meeting Information
Meeting: Meeting of the American Astronomical Society (AAS)
Location: Seattle, WA
Country: United States
Start Date: January 4, 2015
End Date: January 8, 2015
Sponsors: American Astronomical Society
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Instrument
Technology Roadmap
Telescope
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