Alison Nordt,1 Larry Dewell,1 Rodrigo Zeledon,1 Margaret Shaw-Lecerf,1 Matthew Gilbertson,1 Kiarash Tajdaran,1 Alexander Sireci,1 Alex Petrovsky,1 Alyssa Ruiz1
1Lockheed Martin Advanced Technology Ctr. (United States)
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In the next decade, NASA envisions a large space-based telescope that will perform unprecedented astronomy focused on the detection and characterization of Earth-like exoplanets. Recent advances in optical coronography enable this mission, but the technology imposes challenging requirements on telescope dynamic stability and vibration isolation. An integrated non-contact pointing and vibration isolation system called the Disturbance Free Payload (DFP) provides a means to achieve this stability. This system provides an ideal non-contact state (with only residual coupling from power and data cables and actuator effects) while allowing for the necessary degree of rigid-body payload control to meet required telescope pointing and system line-of-sight (LOS) agility. A subscale demonstration of the DFP technology on a CubeSat operating in 6 degrees of freedom in the space environment is one of several developments needed to advance the DFP architecture to TRL 6. This paper describes the mission goals and the preliminary payload and experiment design.
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Alison Nordt, Larry Dewell, Rodrigo Zeledon, Margaret Shaw-Lecerf, Matthew Gilbertson, Kiarash Tajdaran, Alexander Sireci, Alex Petrovsky, Alyssa Ruiz, "Non-contact vibration isolation technology demonstration on a CubeSat," Proc. SPIE 11443, Space Telescopes and Instrumentation 2020: Optical, Infrared, and Millimeter Wave, 1144332 (13 December 2020); https://doi.org/10.1117/12.2563019