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タイトルATLAST-9.2: A Deployable Large Aperture UVOIR Space Telescope
著者(英)Smith, S.; Woodgate, B.; Oegerle, William R.; Lyon, R.; Pasquale, B.; Gong, Q.; Budinoff, J.; Townsend, J.; Thronson, H.; Perrygo, C.; Purves, L.; Hyde, T.; Howard, J.; Ebbets, D.; Bolcar, M.; Feinberg, L.; Jones, A.; Thompson, P.; Gull, T.; Dean, B.; Clampin, N.; Postman, M.
著者所属(英)NASA Goddard Space Flight Center
発行日2010-01-07
言語eng
内容記述We present the results of a study of a deployable version of the Advanced Technology Large Aperture Space Telescope (ATLAST) that could be launched on an Evolved Expendable Launch Vehicle (EELV). ATLAST is a concept for a next-generation UVOIR observatory to follow HST and JWST. The observatory retains significant heritage from JWST, thereby taking advantage of technologies and engineering already developed for that mission. At the same time, we have identified several design changes to the JWST architecture, some of which are required due to the demanding wavefront error requirements at visible wavelengths. The optical telescope assembly has a segmented 9.2-meter aperture and consists of 36 hexagonal glass mirrors, each of which is I.3l5m in size (flat-to-flat). The telescope can be folded to fit in the 6.5m fairing on the planned upgrade to the Delta-IV heavy launch vehicle. Near-real time wavefront sensing and control is performed on-board the telescope using stars in the field of view to deliver diffraction limited imaging performance at 500nm wavelength. The optical design of the telescope provides an 8x20 arcmin FOV in which 4-5 instruments can be accommodated, plus fine guidance and wavefront sensors. Unlike JWST, the OTA sits at the end of a multi-gimbaled arm, allowing pitch and roll motion, and is isolated from the sunshield and spacecraft bus by an active isolation system. Our design permits servicing in order to extend the life of the observatory.
NASA分類Astronomy
権利Copyright


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