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Mars Regolith Properties as Constrained from HP3 Mole Operations and Thermal Measurements

Spohn, Tilman and Grott, Matthias and Müller, Nils and Knollenberg, Jörg and Krause, Christian and Hudson, Troy L. and Deen, R. and Marteau, E. and Golombek, M. and Hurst, K. and Piqueux, S. and Smrekar, S. and Thomas, Ann Louise and Fantinati, Cinzia and Lichtenheldt, Roy and Wippermann, Torben (2020) Mars Regolith Properties as Constrained from HP3 Mole Operations and Thermal Measurements. EGU General Assembly 2020, Online.

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Official URL: https://meetingorganizer.copernicus.org/EGU2020/EGU2020-9163.html

Abstract

The Heat Flow and Physical Properties Package HP3 onboard the Nasa InSight mission has been on the surface of Mars for more than one Earth year. The instrument's primary goal is to measure Mars' surface heat flow through measuring the geothermal gradient and the thermal condunctivity at depths between 3 and 5m. To get to depth, the package includes a penetrator nicknamed the "Mole" equipped with sensors to precisely measure the thermal conductivity. The Mole tows a tether with printed temperature sensors; a device to measure the length of the tether towed and a tiltmeter will help to track the path of the Mole and the tether. Progress of the Mole has been stymied by difficulties of digging into the regolith. The Mole functions as a mechanical diode with an internal hammer mechanism that drives it forward. Recoil is balanced mostly by internal masses but a remaining 3 to 5N has to be absorbed by hull friction. The Mole was designed to work in cohesionless sand but at the InSight landing a cohesive duricrust of at least 7cm thickness but possibly 20cm thick was found. Upon initial penetration to 35cm depth, the Mole punched a hole about 6cm wide and 7cm deep into the duricrust, leaving more than a fourth of its length without hull friction. It is widely agreed that the lack of friction is the reason for the failure to penetrate further. The HP3 team has since used the robotic arm with its scoop to pin the Mole to the wall of the hole and helped it penetrate further to almost 40cm. The initial penetration rate of the Mole has been used to estimate a penetration resistance of 300kPa. Attempts to crush the duricrust a few cm away from the pit have been unsuccessful from which a lower bound to the compressive strength of 350kPa is estimated. Analysis of the slope of the steep walls of the hole gave a lower bound to cohesion of 10kPa. As for thermal properties, a measurement of the thermal conductivity of the regolith with the Mole thermal sensors resulted in 0.045 Wm-1K-1. The value is considerably uncertain because part of the Mole having contact to air. The HP³ radiometer has been monitoring the surface temperature next to the lander and a thermal model fitted to the data give a regolith thermal inertia of 189 ± 10 J m-2 K-1 s-1/2. With best estimates of heat capacity and density, this corresponds to a thermal conductivity of 0.045 Wm-1K-1, consistent with the above measurement using the Mole. The data can be fitted well with a homogeneous soil model, but observations of Phobos eclipses in March 2019 indicate that there possibly is a thin top layer of lower thermal conductivity. A model with a top 5 mm layer of 0.02 Wm-1K-1 above a half-space of 0.05 Wm-1K-1 matches the amplitudes of both the diurnal and eclipse temperature curves. Another set of eclipses will occur in April 2020.

Item URL in elib:https://elib.dlr.de/136416/
Document Type:Conference or Workshop Item (Speech)
Title:Mars Regolith Properties as Constrained from HP3 Mole Operations and Thermal Measurements
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Spohn, TilmanTilman.Spohn (at) dlr.deUNSPECIFIED
Grott, MatthiasMatthias.Grott (at) dlr.deUNSPECIFIED
Müller, NilsNils.Mueller (at) dlr.deUNSPECIFIED
Knollenberg, JörgJoerg.Knollenberg (at) dlr.deUNSPECIFIED
Krause, ChristianChristian.Krause (at) dlr.deUNSPECIFIED
Hudson, Troy L.Troy.L.Hudson (at) jpl.nasa.govhttps://orcid.org/0000-0002-5879-6633
Deen, R.Jet Propulsion Laboratory, California Institute of Technology, Pasadena, USAUNSPECIFIED
Marteau, E.Jet Propulsion Laboratory, Pasadena, CA, USAUNSPECIFIED
Golombek, M.Jet Propulsion Laboratory, Pasadena, CA, USAUNSPECIFIED
Hurst, K.JPL, California Institute of Technology, Pasadena, CA, USAUNSPECIFIED
Piqueux, S.jet propulsion laboratory, california institute of technology (pasadena, ca, 91109)UNSPECIFIED
Smrekar, S.suzanne.e.smrekar (at) jpl.nasa.govUNSPECIFIED
Thomas, Ann LouiseDLR-Köln, louise.thomas (at) dlr.deUNSPECIFIED
Fantinati, CinziaDLR, KölnUNSPECIFIED
Lichtenheldt, RoyRoy.Lichtenheldt (at) dlr.dehttps://orcid.org/0000-0002-2539-4910
Wippermann, TorbenTorben.Wippermann (at) dlr.dehttps://orcid.org/0000-0002-0354-6557
Date:2020
Refereed publication:No
Open Access:Yes
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:InSight HP3 Mars Regolith
Event Title:EGU General Assembly 2020
Event Location:Online
Event Type:international Conference
Organizer:EGU
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space Exploration
DLR - Research area:Raumfahrt
DLR - Program:R EW - Space Exploration
DLR - Research theme (Project):R - Project InSight - HP3
Location: Berlin-Adlershof , Bremen , Köln-Porz , Oberpfaffenhofen
Institutes and Institutions:Institute of Planetary Research
Institute of Planetary Research > Planetary Physics
Space Operations and Astronaut Training > User center for space experiments (MUSC)
Institute of Space Systems
Institute of Space Systems > Land and Exploration Technology
Institute of System Dynamics and Control
Institute of System Dynamics and Control > Space System Dynamics
Deposited By: Grott, Dr.rer.nat. Matthias
Deposited On:06 Oct 2020 07:29
Last Modified:13 Oct 2020 08:00

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