An air-to-air missile is always submitted to extremes conditions of temperature, such as a hot runway in the desert
dropping down to very cold conditions at high altitudes. It is evident that the optical system must be able to provide
satisfactory image quality under any circumstances without causing any major degradation to the image. Under this
perspective, two different designs of optical systems will be considered for this missile: one catadioptric, using a
modified Cassegrain telescope and another one purely dioptric. Both optical systems must be able to focus energy in two
different arrays of detectors, one for the near infrared radiation and the other one for the medium infrared. Due to the
special missile flight profile, the temperature operational range will be determined and considered in order to design and
athermalize the optical systems. Due to the large temperatures range, the missile optical system will experience
deformation effects that will cause defocus and image degradation. A correct choice of materials, including the telescope
body and dome shroud must be determined to minimize the defocus effect. Also a thermal compensator ought to be
strategically placed on both designs to provide focus correction for all the temperatures range. Following that, the optical
designs will be analyzed for effects of stray light and ghost image to find out what are the most suitable absorbing paint
and anti-reflective coatings to be used. In the last step, both systems will be classified accordingly to their characteristics
of performance, weight, size, viability and price and the best will integrate the missile optical system.
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