Abstract
This paper discusses the optical systems of the objectives of optoelectronic cameras
with entrance-pupil diameters of 200-350mm for mini spacecraft and 500-750mm for small spacecraft, developed at OAO LOMO, with angular fields of
2°-4.5°, minimized in mass and size by choosing the
optimum optical systems of the objectives. The objectives use two-mirror layouts
with lens, single-mirror, and mirror-lens field-aberration correctors and
focal-length converters. Versions of the construction of the optical layouts and
their parameters are presented.
© 2009 Optical Society of America
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