Design study of 8 meter monolithic mirror UV/optical space telescope
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The planned Ares V launch vehicle with its 10 meter fairing shroud and 55,000 kg capacity to the Sun Earth L2 point enables entirely new classes of space telescopes. NASA MSFC has conducted a preliminary study that demonstrates the feasibility of launching a 6 to 8 meter class monolithic primary mirror telescope to Sun-Earth L2 using an Ares V. Specific technical areas studied included optical design; structural design/analysis including primary mirror support structure, sun shade and secondary mirror support structure; thermal analysis; launch vehicle performance and trajectory; spacecraft including structure, propulsion, GN&C, avionics, power systems and reaction wheels; operations & servicing; mass and power budgets; and system cost.
[1] H. Philip Stahl. Ares V launch capability enables future space telescopes , 2007, SPIE Optical Engineering + Applications.
[2] Stephen Unwin,et al. Science with an 8-meter to 16-meter optical/UV space telescope , 2008, Astronomical Telescopes + Instrumentation.
[3] Roland Geyl,et al. REOSC contribution to VLT and Gemini , 1999, Optical Systems Design.
[4] H. Philip Stahl,et al. Science Enabled by the Ares V: A Large Monolithic Telescope Placed at the Second Sun-Earth Lagrange Point , 2007 .