Four-Mirror Freeform Reflective Imaging Systems

Metadata Updated: May 2, 2019

Central Objectives: The research involves a revelation of the solution space for revolutionary families of four-mirror freeform reflective imaging systems. A freeform optical system is one that lacks rotational symmetry, meaning there is no constraint on the surface shape of the mirrors. Freeform designs can mitigate the disadvantages that prevent reflective systems from being used in larger field of view applications by yielding unobscured designs and leveraging the added freedom of surface shape to better correct the optical aberrations in the system. Freeform designs are made unobscured by breaking the axis of rotational-symmetry and tilting the individual elements themselves. They do not require an offset aperture or field bias, which brings a unique advantage in the correction of optical aberrations. By getting the mirrors out of their own way, more surfaces can be introduced. When compared to alternate solutions, whether it is a rotationally symmetric system or an unobscured system with the same number of elements, an increased diffraction-limited field of view has been demonstrated in our group's research.

Methods/Techniques: The exploration of the solution space will be accomplished by expanding upon the work of Andrew Rakich, who derived the analytical solution space for four-mirror anastigmat telescopes. The systems that are yielded from his method have spherical surfaces and an axis of rotational symmetry. These designs will be used as starting points for subsequent freeform designs. Lens design software will be used to optimize the design as the elements are tilted. When tilting elements, very strong astigmatism is introduced. Therefore, toroidal base mirrors for the freeform surfaces are needed for correction. Zernike polynomials are then introduced to the toroidal base shapes to further correct the system. The research aims to explore a variety of targeted research questions that aim to address space technology challenges. The sensitivity of the designs from the solution space to common tolerances will be studied using full-field displays that isolate each aberration and show its dependence over the field, combined with Nodal Aberration Theory that puts tolerances in linear space, making the sensitivity calculation efficient and complete. Special attention will be paid to geometries that may be more conducive to stray light reduction through the use of baffles. Similarly, other geometries may be more conducive to radiation shielding by using the mirror substrates themselves as part of the shielding. The added flexibility of folding geometry allows for the design to be tailored to system engineering constraints that could not be addressed with rotationally symmetric systems or unobscured non-freeform systems. Design approaches to achieve these characteristics will be developed.

Significance: This research will address NASA interests as per the July 2015 technology roadmap item TA A key, driving aspect of this work will be to focus on revealing key flat field Large, low cost, lightweight precision monolithic mirrors that provide a high degree of thermal and dynamic stability, and wavefront sensing and control for Ultra-Stable Large-Aperture UV/Visible/Near-IR telescopes. This research is directly relevant to the Observatories level 2 TABS element, 8.2. More specifically, it is relevant to the level 3 TABS element Mirror Systems. The significance of this work is to provide imaging system designs with larger diffraction-limited etendues than the state-of-the-art, (meaning larger apertures and fields of view), which will make the most of limited package sizes and mass constraints. This will advance the optical instrumentation on space probes as well as observatories on the ground towards new space discoveries and knowledge.

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Public: This dataset is intended for public access and use. License: U.S. Government Work

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Metadata Created Date August 1, 2018
Metadata Updated Date May 2, 2019

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Harvested from NASA Data.json

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Resource Type Dataset
Metadata Created Date August 1, 2018
Metadata Updated Date May 2, 2019
Publisher Space Technology Mission Directorate
Unique Identifier TECHPORT_88633
Maintainer Email
Public Access Level public
Bureau Code 026:00
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Datagov Dedupe Retained 20190501230127
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Harvest Source Title NASA Data.json
Data First Published 2020-08-01T07:00:00.000Z
Homepage URL
Language en-US
Data Last Modified 2018-01-10T00:00:00.000Z
Program Code 026:027
Publisher Hierarchy National Aeronautics and Space Administration > Space Technology Mission Directorate
Source Datajson Identifier True
Source Hash 2fee94abece5ce51b7e9f242da4b6b122b37edbe
Source Schema Version 1.1

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