2000
DOI: 10.1117/12.394049
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<title>Integrated modeling of a semirigid hybrid mirror and a highly actuated membrane mirror as candidates for the Next Generation Space Telescope</title>

Abstract: Advanced space telescopes which will eventually replace the Hubble Space Telescope (HST) will have 8-20 m diameter apertures. Primary mirrors (PM's) of these dimensions will fold to fit into the space launcher. By necessity, these mirrors will be extremely lightweight and flexible. The historical approaches to mirror designs, where the mirror is made as rigid as possible to maintain figure and to serve as the anchor for the entire telescope, can no longer be applied. New design concepts and verifications will … Show more

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“…This requires good material characteristics including low coefficient of temperature expansion (CTE), high heat conductivity within the range of temperature drops etc.. In the programs (NMSD, AMSD) of development of the mirror for the NGST [15,24,[37][38][39][40] there were mainly considered two concepts of the mirror's structure.…”
Section: Super-light Mirrorsmentioning
confidence: 99%
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“…This requires good material characteristics including low coefficient of temperature expansion (CTE), high heat conductivity within the range of temperature drops etc.. In the programs (NMSD, AMSD) of development of the mirror for the NGST [15,24,[37][38][39][40] there were mainly considered two concepts of the mirror's structure.…”
Section: Super-light Mirrorsmentioning
confidence: 99%
“…The structural, thermal and optical properties of the both types of the mirror were investigated in [37]. 1) As an example of a semi-rigid hybrid mirror for the demonstrator can be a circular mirror 1.6 m in diameter described in [20].…”
Section: Super-light Mirrorsmentioning
confidence: 99%
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