Thermal Sensitivity Study of Lunar Terrain Vehicle WheelsSince the early development of lunar vehicles for the Apollo program, designing a wheel capable of functioning in the harsh equatorial lunar environment was identified as a uniquely difficult engineering challenge. The Lunar Terrain Vehicle (LTV) must contend with many of the same challenges encountered during the Apollo missions, but with the addition of colder, more complex thermal environments at the lunar south pole and longer Artemis mission timelines. A full thermal assessment of LTV wheels should capture these and other details to assess heat leak through the wheels and extreme hot and cold temperatures. The goals of this study are to provide bounding lunar south pole thermal environments; to define sensitivity to interactions between the wheel and the lunar surface in different operation modes, such as parked and traversing; and to identify thermal performance concerns related to the use of shape memory alloys.
Document ID
20240006096
Acquisition Source
Johnson Space Center
Document Type
White Paper
Authors
William Birmingham (Jacobs (United States) Dallas, Texas, United States)
Date Acquired
May 13, 2024
Publication Date
May 20, 2024
Subject Category
Spacecraft Design, Testing and PerformanceEngineering (General)
Funding Number(s)
WBS: 007686.06.01.02.72
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Lunar Terrain VehicleRovertiresconductionlunar regolithLunar South Pole thermal environmentshape memory alloythermal modeling