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:: Design overview
Since 1999, various concept studies for the
instrument have been carried out sponsored by ESA and NASA
(see reports by Wright et al. 1999, Serabyn et al. 1999, MISC
report). The earlier studies had 4–6 modules in the
instrument, with two modules each for the camera and spectroscopy
channels to accomodate different plate scales and cope with
the different background levels.
The most recent studies focussed on simplification
and lightweighting of the instrument; the minimum design that
satisfies all the science goals has just one module each for
the camera and spectrometer, plus a module containing the
common fore-optics, with a minimum number of mechanisms. For
the spectroscopy channel, both traditional long-slit designs
and more innovative integral-field units (IFU) have been considered.
From the science point of view, an IFU is preferred and is
endorsed by the MISC report and incorporated in the current
design baseline.
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Scrall
image to identify elements or click to enlarge.
+ Structural concept of the OM: view
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An optical pre-design study of this system has been
made, primarily at Service d'Astrophysique (SAP, Saclay, France)
for the camera subsystem and at the UK Astronomy Technology Centre
(ATC, Royal Observatory, Edingburgh, UK) for the spectrograph. All
optical elements (except filters and grisms) are reflective.
This system not only provides the basic imaging mode, but
also the coronographic mode and the low-resolution R ~ 100 spectroscopy.
The latter mode is fed from the camera optics and uses low-dispersion
grisms. All three modes make use of the same high flux level detector;
in the present design this is a single 1024 x 1024 (1K x 1K) array
of 27 x 27 µm2 pixel size with a single pixel field of view
of 0.1'', chosen to be Nyquist sampled at ~8 µm.
This module provides 'high-resolution' spectroscopy in integral-field
mode, using 4 parallel wavelength channels. The spectrometer has
its own low flux level detectors. Most of the Dutch effort will
go in the design, building of this spectrometer sub-instrument.
See bloc diagram.
The studies and the current design have drawn heavily
on the European experience in building mid-infrared instruments
for ISO, Herschel and for ground-based telescopes such as the VLT
(VISIR), UKIRT (image-slicer) and Gemini (MICHELLE). In fact, most
of the elements have already been incorporated in a similar form
in other instruments. Thus, the risk in the design and development
is minimized in this approach.
The heart of the instrument is formed by the detectors.
Here the NGST project profits heavily from the detector development
for SIRTF, which has produced 256 x 256 pixel formats with high
quantum efficiency and encouragingly low dark currents. The NASA-JWST
project has funded development to extend the detector device format
to 1024 x 1024 pixels, with the aim to also bring down the read-noise
and dark currents to levels such that JWST is background limited
at low spectral resolution as short as 6 µm.
Thanks to these rapid developments in mid-infrared
detector arrays, the enormous jump forward in sensitivity and observing
speed is possible; indeed, there are few other wavelength ranges
where such large improvements can still be achieved. The detectors
for the camera and spectrometer will be procured by the US part
of the consortium.
For optimal performance and reduction of thermal
background emission, the optics should be as cold as possible (
<24 K), with an enclosure temperature of ~18 K and the detectors
themselves cooled to < 7.5 K. This will be accomplished by a
solid-hydrogen cryostat, to be procured by ESA.
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