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Modular Active Self-Assembling Space Telescope SwarmsThe Phase I study included a detailed exploration of a specific mission concept based on this architecture - a 31-meter diameter version of the LUVOIR (Large Ultraviolet Optical Infrared Surveyor) mission concept with the same wavelength coverage and wave-front quality requirements. The study focused on establishing the feasibility of the proposed concept with respect to what were identified as the most challenging aspects of the mission: the ability to find orbital solutions using solar sail propulsion for both the initial transfers and subsequent rendezvous trajectories; and the ability to generate the required final primary mirror surface out of uniformly polished individual module mirrors using deformation via mechanical degrees of freedom. As a result of the Phase I work it was shown that both orbital and optical solutions are feasible, but will require technology advancement in multiple key areas. In particular, improvements to solar sail areal densities and loading factors will allow us to more easily find fully general solutions for the transfer trajectories, while lower mass, ultra-precise cryogenic linear actuators will likely be needed to form the final mirror shape. However, it was found that current state of the art in solar sails was sufficient for rendezvous trajectories once on-orbit, that the requisite wave-front quality could be achieved with actuation requirements not more stringent than those being carried by LUVOIR, and that there exists a well-defined design space in which the module spacecraft designs can be optimized. The technology development required to progress this work overlaps significantly with numerous NASA technology roadmaps, as well as the Exoplanet Exploration Program's technologies gap list, meaning that continued development of this concept would directly benefit a variety of NASA programs, as well as enabling the completely unique capabilities provided by a 31-meter optical space telescope...Our architecture requires only a single module type allowing us to directly leverage the cost and efficiency benefits of true mass production, in direct contrast to previously explored self-assembling swarm concepts, which typically include multiple module types.
Document ID
20190018062
Acquisition Source
Headquarters
Document Type
Contractor or Grantee Report
Authors
Savransky, Dmitry
(Cornell Univ. Ithaca, NY, United States)
Keithly, Dean
(Cornell Univ. Ithaca, NY, United States)
Shapiro, Jacob
(Cornell Univ. Ithaca, NY, United States)
Soto, Gabriel
(Cornell Univ. Ithaca, NY, United States)
Gustafson, Erik
(Cornell Univ. Ithaca, NY, United States)
Liu, Kevin
(Cornell Univ. Ithaca, NY, United States)
Della Sanatina, Christopher
(Cornell Univ. Ithaca, NY, United States)
Date Acquired
May 10, 2019
Publication Date
January 1, 2019
Subject Category
Astronomy
Optics
Report/Patent Number
HQ-E-DAA-TN67902
NIAC 17-NIAC18B-0165
Report Number: HQ-E-DAA-TN67902
Report Number: NIAC 17-NIAC18B-0165
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Technical Review
NASA Technical Management
Keywords
Astronomy
Exploration
Orbital
Swarms
Mission
Modular
Optical Solutions
Telescope
Self-Assembling
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