2010
DOI: 10.1016/j.actaastro.2009.07.025
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Large aperture telescopes for launch with the Ares V launch vehicle

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Cited by 6 publications
(3 citation statements)
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“…In the present landscape, space-deployable membrane structures are based on mechanical deployment [12,13], inflatable deployment [14], and elastic deployment [15]. These deployment methods are susceptible to constraints such as complexity, mechanical failures, and limitations related to weight and volume.…”
Section: Introductionmentioning
confidence: 99%
“…In the present landscape, space-deployable membrane structures are based on mechanical deployment [12,13], inflatable deployment [14], and elastic deployment [15]. These deployment methods are susceptible to constraints such as complexity, mechanical failures, and limitations related to weight and volume.…”
Section: Introductionmentioning
confidence: 99%
“…Increased performance can be achieved by increasing the telescope aperture, since a telescope's spatial resolution increases linearly with its diameter (D), its collecting area is proportional to D 2 , and its sensitivity increases as D 4 . The size of the launch vehicle's payload fairing is a limiting factor for the size of space telescope, but telescope apertures ~1.7 to 2.4 times the fairing diameter can be achieved by carefully folding the telescope for launch and autonomously deploying it once reaching orbit [1].…”
Section: Introductionmentioning
confidence: 99%
“…A segmented primary mirror stitches serial arrays of sub-mirrors together to reach the optimal capabilities of a monolithic mirror. This type of space telescope can be folded for launch and deploy autonomously after reaching orbit [ 2 ]. However, high-quality images equivalent to those of a monolithic mirror can only be achieved if co-phasing of the segmented mirrors occurs.…”
Section: Introductionmentioning
confidence: 99%