Proc. SPIE 5904-18 (2005)
Fujishiro, et al.
Abstract:
The MIR-L is the mid-IR (12--26 μm) instrument for Japanese infrared astronomical satellite, the ASTRO-F.
The instrument has 2 observing modes: a wide field imaging mode with a field of view of 10.7×10.2 arcmin^2
and a low resolution spectroscopic mode with a spectral resolution R ~ 20.
The spectroscopic mode provides with not only slit-spectroscopy for extended sources but also
slitless-spectroscopy for point sources.
We describe here the design, manufacturing, and performance evaluation of the cryogenic optical
system of the MIR-L.
The concept of the optical system design is to realize wide field observations with a compact size.
The instrument employs a refractive optics of 5 lenses (CsI - CsI - KRS-5 - CsI - KRS-5) with a
256×256 pixel Si:As IBC array detector, 3 filters, and 2 grisms.
The refractive indices of CsI and KRS-5 at the operating temperature of about 6 K have ambiguities
because of the difficulty of the measurements.
We therefore designed the MIR-L optics with tolerances for the uncertainties of the indices.
Since both CsI and KRS-5 have the fragility and the large thermal expansion,
we designed a specialized mounting architecture to prevent from making damages and/or
decentrations of the lenses atcryogenic temperatures under the serious vibration during the launch.
As a result, the optical system of the MIR-L has passed both vibration and thermal cycle tests
without damage and performance degradation,
and achieved diffraction limited performance over its full wavelength range at the operating
temperature.