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OCCAMS: Optically Controlled and Corrected Active Meta-Material Space StructuresTelescopes require sub-wavelength figure (shape) error in order to achieve acceptable Strehl ratios. Traditional methods of achieving this require rigid and therefore heavy mirrors and reaction structures as well as proportionally heavy and expensive spacecraft busses and launch vehicles. This effectively limits the diameter and therefore resolution and collecting area of space optics. Large diameter telescopes must either be heavy or actively controlled. Space telescopes of the size proposed for missions such as TPF (Terrestrial Planet Finder), TPI (Terrestrial Planet Imager), etc. will likely require large active primaries and structures and corrective optics to implement downstream wavefront control. We propose a novel viable enabling technology. High resolution space imaging requires the production of lightweight large aperture optics subject to design tradespace constraints based on nanometer physical tolerances, low system aerial density, high control authority, suitable thermal and mechanical properties, deployment capability, launch vehicle volume constraints, as well as production cost and schedule risk mitigation. Segmented systems impose additional requirements on segment alignment, wavefront phasing, and telescope mass with increased edge diffraction. Photons weigh nothing. Why must even small space telescopes "weigh" tons? Our team is working to demonstrate that they do not, by leveraging 15 years of effort and a novel advanced concept.The ultimate research goal is to refine technology to produce a mission capable ultra-lightweight membrane optic whose shape can be remotely controlled using a laser beam. Using our novel optically-controlled molecular actuators allows substitution of optically-induced control for rigidity and mirror mass. In analogy with noise-canceling headphones, this technique also potentially provides a way to excite vibratory modes to couple with and damp out normal modes of oscillation induced by slewing, other motion and thermal changes, thus allowing a robust response to repointing of a large aperture.
Document ID
20190001173
Acquisition Source
Headquarters
Document Type
Other
Authors
Ritter, Joe
(Neoteric Physics, Inc. Kihei, HI, United States)
Date Acquired
March 4, 2019
Publication Date
September 7, 2014
Subject Category
Composite Materials
Report/Patent Number
HQ-E-DAA-TN63104
NEOTERIC Physics PR No. 4200450254
Report Number: HQ-E-DAA-TN63104
Report Number: NEOTERIC Physics PR No. 4200450254
Funding Number(s)
CONTRACT_GRANT: NNX12AQ56G
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Keywords
Astronomy
Optics
Photons
Structures
Telescopes
Vibration
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