TY - GEN
T1 - Approaches to lowering the cost of large space telescopes
AU - Douglas, Ewan S.
AU - Aldering, Greg
AU - Allan, Greg W.
AU - Anche, Ramya
AU - Angel, Roger
AU - Ard, Cameron C.
AU - Chakrabarti, Supriya
AU - Close, Laird M.
AU - Derby, Kevin
AU - Edelstein, Jerry
AU - Ford, John
AU - Gersh-Range, Jessica
AU - Haffert, Sebastiaan Y.
AU - Ingraham, Patrick J.
AU - Kang, Hyukmo
AU - Kelly, Douglas M.
AU - Kim, Daewook
AU - Lesser, Michael
AU - Leisenring, Jarron M.
AU - Lin, Yu Chia
AU - Males, Jared R.
AU - Martin, Buddy
AU - Payan, Bianca Alondra
AU - Sai Krishanth, P. M.
AU - Rubin, David
AU - Selznick, Sanford
AU - Van Gorkom, Kyle
AU - Jannuzi, Buell T.
AU - Perlmutter, Saul
N1 - Publisher Copyright:
© 2023 SPIE.
PY - 2023
Y1 - 2023
N2 - New development approaches, including launch vehicles and advances in sensors, computing, and software, have lowered the cost of entry into space, and have enabled a revolution in low-cost, high-risk Small Satellite (SmallSat) missions. To bring about a similar transformation in larger space telescopes, it is necessary to reconsider the full paradigm of space observatories. Here we will review the history of space telescope development and cost drivers, and describe an example conceptual design for a low cost 6.5 m optical telescope to enable new science when operated in space at room temperature. It uses a monolithic primary mirror of borosilicate glass, drawing on lessons and tools from decades of experience with ground-based observatories and instruments, as well as flagship space missions. It takes advantage, as do large launch vehicles, of increased computing power and space-worthy commercial electronics in low-cost active predictive control systems to maintain stability. We will describe an approach that incorporates science and trade study results that address driving requirements such as integration and testing costs, reliability, spacecraft jitter, and wavefront stability in this new risk-tolerant “LargeSat” context.
AB - New development approaches, including launch vehicles and advances in sensors, computing, and software, have lowered the cost of entry into space, and have enabled a revolution in low-cost, high-risk Small Satellite (SmallSat) missions. To bring about a similar transformation in larger space telescopes, it is necessary to reconsider the full paradigm of space observatories. Here we will review the history of space telescope development and cost drivers, and describe an example conceptual design for a low cost 6.5 m optical telescope to enable new science when operated in space at room temperature. It uses a monolithic primary mirror of borosilicate glass, drawing on lessons and tools from decades of experience with ground-based observatories and instruments, as well as flagship space missions. It takes advantage, as do large launch vehicles, of increased computing power and space-worthy commercial electronics in low-cost active predictive control systems to maintain stability. We will describe an approach that incorporates science and trade study results that address driving requirements such as integration and testing costs, reliability, spacecraft jitter, and wavefront stability in this new risk-tolerant “LargeSat” context.
KW - CubeSats
KW - LargeSats
KW - Space telescopes
UR - http://www.scopus.com/inward/record.url?scp=85176278338&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=85176278338&partnerID=8YFLogxK
U2 - 10.1117/12.2677843
DO - 10.1117/12.2677843
M3 - Conference contribution
AN - SCOPUS:85176278338
T3 - Proceedings of SPIE - The International Society for Optical Engineering
BT - Astronomical Optics
A2 - Hull, Tony B.
A2 - Kim, Daewook
A2 - Hallibert, Pascal
PB - SPIE
T2 - Astronomical Optics: Design, Manufacture, and Test of Space and Ground Systems IV 2023
Y2 - 21 August 2023 through 24 August 2023
ER -