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Mechanical Design and Operation of a Novel Lunar Environment Structural Test Rig (LESTR)The Lunar Environment Structural Test Rig (LESTR) was developed to address a critical gap in mechanical property data for metal alloy wire materials under lunar-relevant conditions down to 40 K. Conventional aerospace material databases provide thermophysical properties for bulk metals over a wide temperature range, but validated mechanical and physical property data below 77 K, particularly for small-diameter wires, remain limited and are generally the exception rather than the rule. These conditions are essential for Artemis mission hardware such as shape memory alloy (SMA) rover tires. LESTR’s design requirements were to combine a high-stiffness electrodynamic load frame with closed- cycle cryogenic cooling, high-vacuum capability (10–6 torr), and noncontact optical strain measurement to enable tensile, four-point bend, and fatigue testing of wires or other materials and geometries at temperatures from 40 to 125 K. These considerable requirements were merged with the need to lower the barrier of testing for the end user as measured in terms of cost-per-test cycle, safety improvement, and reduction in upkeep costs associated with state-of-the-art solutions associated with cryomechanical material characterization. The system incorporates modular gripping and alignment fixtures; precision thermal management using cryocoolers and embedded heaters; and integrated instrumentation for displacement, load, temperature, and vacuum control. Calibration procedures establish correlations between tooling and specimen temperature, ensuring accurate thermal conditions across the design envelope unbound by cryofluid conditions in heritage immersion-based test systems. Initial validation tests using Inconel (Special Metals Corp.) wire demonstrated accurate ultimate strength and post-yield behavior. The load frame operation was also verified under representative service conditions, including thermal cycling and prolonged fatigue loading. By generating mechanical property data at ultralow temperatures, LESTR fills a critical gap in existing materials databases and provides a scalable platform for iterative alloy development and durability assessment for planetary hardware. This capability supports NASA’s long-term objectives for surface exploration by enabling design confidence for components operating in extreme cryogenic environments.
Document ID
20260005630
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Heather A Oravec
(University of Akron Akron, United States)
Adam Rice
(HX5, LLC)
Ariel Dimston
(Glenn Research Center Cleveland, United States)
Jason Wendell
(Glenn Research Center Cleveland, United States)
Wesley Johnson
(Glenn Research Center Cleveland, United States)
Jan Sobon
(Glenn Research Center Cleveland, United States)
Andrew Ring
(Glenn Research Center Cleveland, United States)
Michael Lewis
(NASA Retired Cleveland, Ohio, United States)
Santo Padula
(Glenn Research Center Cleveland, United States)
Date Acquired
June 22, 2026
Publication Date
September 1, 2026
Publication Information
Publisher: National Aeronautics and Space Administration
Subject Category
Engineering (General)
Report/Patent Number
NASA/TM-20260005630
E-20428
Funding Number(s)
CONTRACT_GRANT: 80GRC020D003
Distribution Limits
Public
Copyright
Public Use Permitted.
Patent
LEW-20642-1 - Low Temperature SMA Mechanical Testing Apparatus
Patent Application
Technical Review
Single Expert
Keywords
LESTR
Cryogenic Material Characterization
materials for extreme environments
shape memory alloy
cryogenic
four-point bend testing
tensile testing
strain measurement
Lunar environment
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