Design, implementation, and performance of the primary reflector for SALTUS

The Single Aperture Large Telescope for Universe Studies (SALTUS) is a mission concept for a far-infrared observatory developed under the recent Astrophysics Probe Explorer opportunity from the National Aeronautics and Space Administration. The enabling element of the program is a 14-m diameter inflatable primary mirror, M1. Due to its importance to SALTUS and potentially other space observatories, we focus entirely on M1. We present a historical overview of inflatable systems, illustrating that M1 is the logical next step in the evolution of such systems. The process of design and manufacture is addressed. We examine how M1 performs in its environment in terms of the operating temperature, interaction with the solar wind, and shape change due to non-penetrating particles. We investigate the longevity of the inflatant in detail, show that it meets mission lifetime requirements with ample margin, and discuss the development and testing to realize the flight M1.

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Publication Details

Journal
Journal of Astronomical Telescopes Instruments and Systems
Published
2024-09-09
DOI
https://doi.org/10.1117/1.jatis.10.4.042306
Citations
6
Primary Topic
Particle accelerators and beam dynamics
Type
article
Field-Weighted Citation Impact
7.79
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article

Design, implementation, and performance of the primary reflector for SALTUS

Jonathan W. Arenberg, Bob Chang, Leon K. Harding, Daewook Kim et al.
6 citations
Journal of Astronomical Telescopes Instruments and Systems
Particle accelerators and beam dynamics
7.79
article

Design, implementation, and performance of the primary reflector for SALTUS

Jonathan W. Arenberg, Bob Chang, Leon K. Harding, Daewook Kim, Christopher Walker, M. N. Villarreal, Zach Lung, Dave Lung, Steve Kuehn, Arthur Palisoc, Dave Oberg
article en
6 citations

Abstract

The Single Aperture Large Telescope for Universe Studies (SALTUS) is a mission concept for a far-infrared observatory developed under the recent Astrophysics Probe Explorer opportunity from the National Aeronautics and Space Administration. The enabling element of the program is a 14-m diameter inflatable primary mirror, M1. Due to its importance to SALTUS and potentially other space observatories, we focus entirely on M1. We present a historical overview of inflatable systems, illustrating that M1 is the logical next step in the evolution of such systems. The process of design and manufacture is addressed. We examine how M1 performs in its environment in terms of the operating temperature, interaction with the solar wind, and shape change due to non-penetrating particles. We investigate the longevity of the inflatant in detail, show that it meets mission lifetime requirements with ample margin, and discuss the development and testing to realize the flight M1.

Journal of Astronomical Telescopes Instruments and SystemsVol. 10(04)
University of Arizona (US), Northrop Grumman (United States) (US), L.Garde (United States) (US)
Openalex Percentile: Top 3%
Particle accelerators and beam dynamics
7.79
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