of a prototype, called REFIR-BB,
has been funded in 2001 by ASI
with the project called “R&D
bread-board for a FTS to remotely sense the rotational water vapour
(100-1000 cm-1)”. In the first year of activity the hardware
of the prototype has been developed.
has been developed at IFAC-CNR with the collaboration of IMAA-CNR.
The chosen optical configuration of the interferometer follows the
indications raised by EU study of the space mission. It is a
polarising interferometer with a new optical scheme that is able to
meet all the requirements pointed out by the space mission.
configuration is described in more details by B.Carli et al.,
Appl.Opt. 38, pp.3945-3950 (1999). It makes use of four
beam splitters (BS) and provides all the desired features including
broad spectral coverage, two separated input ports
and two output ports, optical compensation for tilt errors in the
moving mirror unit, measurement of the overall input signal (both
planes of polarization) on the same detector. This optical
configuration maximizes the reliability of the spectrometer in
particular for long lifetimepace
applications and optimizes its performances for room temperature
most critical components of the instrument to test with the
experiment are fou wire-grid photolithographic
polarisers for FIR applications and two DLATGS room-temperature
detectors. The polarisers are supplied by the University of Wales,
UK, and by ESA (under the ESTEC contract N. 15612/01/NL/SF:
for REFIR Far-IR interferometry''). The
two detectors are supplied by BAE Systems.
summary of the main parameters that characterize REFIR-BE are
reported in the following Table.
with double input/output port
| 100-1100 cm-1
cm-1 (double-sided interferogram), 0.1 cm-1(single-sided
1.3 mW/m2 sr cm-1 at 400 cm-1
|62cm diameter X 26cm
can be divided into five main subsystems that can be seen in the
following Figure; the interferometer, the pyroelectric detector unit
(PDU), the radiometric calibration system (RCU and RBB),
the reference laser system (RLS), and the data acquisition and
control system (ACS), not shown in the figure.
of the opto-mechanical layout of the instrument.
FIR interferometer is the main unit and includes the beam splitter
unit (BSU), the roof-top-mirror unit (RTMU) on the flexural
translation stage. The figure also shows the RLS sharing the same
path as the FIR interferometer and
the PDU with the two pyroelectric detectors assembled at the output
of the collecting optics. The RCS is composed of three black body
(BB) sources, a reference BB (RBB) in front of the first input port
and a calibration unit (RCU) in
front of the measurement channel. The RCU has an hot BB, a cold BB
and a folding mirror that allows to switch between these two
references sources and the unknown radiance emitted from the observed.
The ACS includes electronical interfaces both for the acquisition of
signals and for the control of the overall instrument operations.
Signals are three high-resolution low-frequency signals for the two
output FIR interferograms and
the reference laser, and 32 low-resolution low-frequency signals for
house-keeping (HK) informations. All the operations are controlled by
PC-based electronics with LabView software. Acquisition cards are one
ICS-610-4 24-bit resolution for the main signals and one NI-PCI-6033-E
16-bit resolutions for the HKs. The
following Picture shows the spectrometer.