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Compact, Deep-Penetrating Geothermal Heat Flow Instrumentation for Lunar LandersGeothermal heat flow is obtained as a product of the two separate measurements of geothermal gradient in, and thermal conductivity of, the vertical soi/rock/regolith interval penetrated by the instrument. Heat flow measurements are a high priority for the geophysical network missions to the Moon recommended by the latest Decadal Survey [I] and previously the International Lunar Network [2]. The two lunar-landing missions planned later this decade by JAXA [3] and ESA [4] also consider geothermal measurements a priority.
Document ID
20120015991
Acquisition Source
Goddard Space Flight Center
Document Type
Conference Paper
Authors
Nagihara, S.
(Texas Technological Univ. Lubbock, TX, United States)
Zacny, K.
(Honeybee Robotics, Inc. Pasadena, CA, United States)
Hedlund, M.
(Honeybee Robotics, Inc. Pasadena, CA, United States)
Taylor, P. T.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
August 26, 2013
Publication Date
October 10, 2012
Subject Category
Lunar And Planetary Science And Exploration
Report/Patent Number
GSFC.ABS.6580.2012
Report Number: GSFC.ABS.6580.2012
Meeting Information
Meeting: International Workshop on Instrumentation for Planetary Missions
Location: Greenbelt, MD
Country: United States
Start Date: October 10, 2012
End Date: October 12, 2012
Distribution Limits
Public
Copyright
Public Use Permitted.
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