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Towards Erecting Straighter Lightweight Towers on the Moon Using Deployable Guy WiresThis paper reports our static stability test findings for a simple guy wire system to correct the natural lateral deflections of an 8.5m tall, compact deployable composite tower intended to support exploration of lunar permanently shadowed regions by nearby robotic assets. Deployable composite booms with microgravity flight heritage are currently being investigated at NASA Langley Research Center (LaRC) and Massachusetts Institute of Technology(MIT)’s Space Resources Workshop for their potential to be vertically deployed in the lunar gravity field, in support of NASA’s Artemis campaign. These applications include vertical solar arrays and the provision of elevated lines-of-sight to science or engineering payloads on landers and rovers, in support of nearby or distant crewed or robotic assets exploring scientifically interesting and hard to reach areas. Useful elevated payloads include radio repeaters, remote sensing and imaging, navigation and power beaming systems. However, while these lightweight booms have an excellent height to mass ratio, they typically exhibit slight axial curvature upon deployment resulting in appreciable lateral dead-load deflection of the tip mass relative to the tower base. This static deflection increases with tower height and tip mass, not only constraining the value delivered by the tower but also endangering its integrity. To develop a competitive, lightweight deployable composite boom tower, a capability to correct static deflections during and after deployment may be required. This paper presents a pathfinder deployable guy wire stability system for the MIT / LaRC self-erecting composite boom lunar tower that provides real time measurements, maintains tension passively, and can serve as a reconfigurable platform to test new guy wire components, configurations and control algorithms. Using a validated, calibrated photogrammetry system, the natural lateral deflection of the boom tip relative to the boom base at different deployed heights in Earth’s gravity field was recorded. With real-time tension measurements it was found that guy wires can significantly reduce the tip deflection of a deployable composite boom under dead load. Specifically, we found that (1) control capability is greatest where it is needed most, i.e. for the lever arm closest to being opposite the direction of deflection, and (2) for a tower height of at least 8.5 m and arm length of at least 60 cm, a solution of differential tension in all three arms exists and, in principle, provides sufficient control capability to correct or significantly reduce boom deflections. We also found that natural deflections occur almost entirely out-of-plane of the seams of the boom cross-section, which was expected, and that the natural boom tip lateral deflection under dead load upon deployment was ~5% of boom deployed length, unexpectedly exceeding the manufacturing acceptance specification of 1%.Ongoing and future collaborative work between LaRC and MIT includes the further investigation of the unexpected lateral deflection, testing of alternative guy wire system designs at higher tensions and higher deployed heights, as well as trade studies of costs and benefits of an optimized integrated guywire system compared to other types of static stability solutions.
Document ID
20210022705
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Alex S Miller
(Massachusetts Institute of Technology Cambridge, Massachusetts, United States)
Joshua Rohrbaugh
(Massachusetts Institute of Technology Cambridge, Massachusetts, United States)
Emma K. Rutherford
(Massachusetts Institute of Technology Cambridge, Massachusetts, United States)
Natasha Stamler
(Massachusetts Institute of Technology Cambridge, Massachusetts, United States)
Benjamin Martell
(Massachusetts Institute of Technology Cambridge, Massachusetts, United States)
George Lordos
(Massachusetts Institute of Technology Cambridge, Massachusetts, United States)
Juan M Fernandez
(Langley Research Center Hampton, Virginia, United States)
Matthew K Chamberlain
(Langley Research Center Hampton, Virginia, United States)
Jeffrey A Hoffman
(Massachusetts Institute of Technology Cambridge, Massachusetts, United States)
Date Acquired
October 12, 2021
Subject Category
Spacecraft Design, Testing And Performance
Meeting Information
Meeting: IEEE Aerospace Conference
Location: Big Sky, MT
Country: US
Start Date: March 5, 2022
End Date: March 12, 2022
Sponsors: Institute of Electrical and Electronics Engineers
Funding Number(s)
PROJECT: 969115.04.28.23.01
Distribution Limits
Public
Copyright
Use by or on behalf of the US Gov. Permitted.
Technical Review
Single Expert
Keywords
lunar towers
guy wires
composite booms
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