32
namely the visible-short-wave infrared from 0.45 to 2.35
um, where the instrument works as an imaging
spectrometer with a spectral resolution of about 10 nm and
the thermal infrared range from 8 to 12.3 um, divided into 3
spectral bands with a typical width of 1 um, where the
instrument works as an imaging radiometer. The spatial
resolution at nadir is about 50 m over a swath (image size)
of 50 km. Access to any site on earth could be provided
within three days (ESA ESAC, 1996).
In order to support such activities, ESA has identified the
necessity to initiate appropriate studies and measurement
campaigns. In this frame, the presented paper discusses a
study that concentrates on the definition of an airborne
imaging spectrometer which could represent a precursor of
the spaceborne instrument and which will therefore be
named APEX (Airborne PRISM Experiment)(Del Bello,
1995).
APEX is a project to develop an airborne PRISM simulator
which will contribute to the
* preparation,
* calibration,
A
Protective
Window
* validation,
* simulation, and
* application development
of the PRISM mission. In addition APEX will be an
advanced imaging spectrometer serving as a testbed for
other imaging spectroscopy applications (Itten, 1997).
2. THE APEX INSTRUMENT
APEX will be an instrument with the following uniqueness
in technical, usage and applications standpoint:
e pushbroom imager with approx. 1000 pixels across
track and a swath width of 2.5 — 5 km
* spectral wavelength range covering 450 — 2500 nm
* 200 user selectable and predefined bands, adapted to the
specific mission and application
* a spectral sampling interval « 15 nm at a spectral
sampling width « 1.5 times the sampling interval
* provides calibrated data and a suite of user oriented
products up to fully geocoded and calibrated data.
Figure 1. APEX Block Diagram
2.1 The Imaging Spectrometer Optomechanical
Subsystem
The ground imager maps the ground (swath of £14°) on
the spectrometer slit of 50 mm height and 0.05 mm
width. High image performance is required in order to
provide maximum energy throughput at the slit and to
define the swath width precisely. The ground image has
to be colour corrected in the total spectral range between
450 and 2500 nm. Behind the ground imager a beam
splitter will be placed to separate the spectral range in a
visual and an IR channel. The use of a beam splitter in
front of the collimators allows to choose more suitable
glasses for the colour correction and for improving the
transmission within the reduced number of spectral
bands. The two collimators project the light coming from
the slit towards the dispersive elements of the
spectrometers.
Prisms will be selected as dispersing elements. The light
scattering in a system containing gratings is considered to
be a risk that cannot be taken. For the visual channel, the
prism materials CaF2 / ZnS are selected, for the IR
channel the prism materials are CaF2 and Sapphire.
International Archives of Photogrammetry and Remote Sensing. Vol. XXXII, Part 7, Budapest, 1998