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MOMA: the challenge to search for organics and biosignatures on Mars

Published online by Cambridge University Press:  13 July 2016

W. Goetz*
Affiliation:
MPS, Göttingen, Germany
W. B. Brinckerhoff
Affiliation:
NASA GSFC, Greenbelt, MD, USA
R. Arevalo Jr.
Affiliation:
NASA GSFC, Greenbelt, MD, USA
C. Freissinet
Affiliation:
NASA GSFC, Greenbelt, MD, USA
S. Getty
Affiliation:
NASA GSFC, Greenbelt, MD, USA
D. P. Glavin
Affiliation:
NASA GSFC, Greenbelt, MD, USA
S. Siljeström
Affiliation:
SP Technical Research Institute of Sweden, Borås, Sweden
A. Buch
Affiliation:
LPGM, Ecole Centrale Paris, Chatenay-Malabry, France
F. Stalport
Affiliation:
LISA, U. Paris-Est, Créteil, U. Paris Diderot, Paris, CNRS, France
A. Grubisic
Affiliation:
NASA GSFC, Greenbelt, MD, USA
X. Li
Affiliation:
NASA GSFC, Greenbelt, MD, USA
V. Pinnick
Affiliation:
NASA GSFC, Greenbelt, MD, USA
R. Danell
Affiliation:
Danell Consulting, Winterville, NC, USA
F. H. W. van Amerom
Affiliation:
Mini-Mass Consulting, Hyattsville, MD, USA
F. Goesmann
Affiliation:
MPS, Göttingen, Germany
H. Steininger
Affiliation:
MPS, Göttingen, Germany
N. Grand
Affiliation:
LISA, U. Paris-Est, Créteil, U. Paris Diderot, Paris, CNRS, France
F. Raulin
Affiliation:
LISA, U. Paris-Est, Créteil, U. Paris Diderot, Paris, CNRS, France
C. Szopa
Affiliation:
LATMOS, Guyancourt, France
U. Meierhenrich
Affiliation:
U. Nice, France
J. R. Brucato
Affiliation:
INAF – Astrophysical Observatory of Arcetri, Firenze, Italy
the MOMA Science Team
Affiliation:
MPS, Göttingen, Germany NASA GSFC, Greenbelt, MD, USA SP Technical Research Institute of Sweden, Borås, Sweden LPGM, Ecole Centrale Paris, Chatenay-Malabry, France LISA, U. Paris-Est, Créteil, U. Paris Diderot, Paris, CNRS, France Danell Consulting, Winterville, NC, USA Mini-Mass Consulting, Hyattsville, MD, USA LATMOS, Guyancourt, France U. Nice, France INAF – Astrophysical Observatory of Arcetri, Firenze, Italy U. Bremen, Germany
*
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Abstract

This paper describes strategies to search for, detect, and identify organic material on the surface and subsurface of Mars. The strategies described include those applied by landed missions in the past and those that will be applied in the future. The value and role of ESA's ExoMars rover and of her key science instrument Mars Organic Molecule Analyzer (MOMA) are critically assessed.

Information

Type
Research Article
Copyright
Copyright © Cambridge University Press 2016 
Figure 0

Fig. 1. Signs of liquid water on (ancient and modern) Mars, (roughly) sorted according to increasing magnification: (a) Example of ancient (noachian) dissected valley networks on Mars’ southern hemisphere. Warrego Vallis may be among the most dissected ones (Ansan & Mangold 2006; Carr 2012). (b) Example of (mostly hesperian) outflow channels with young gullies (c) on the channel wall. (d) Recurring Slope Lineae (RSL) on the wall of a crater in Melas Chasma (part of Valles Marineris) (McEwen et al., 2014). (e) Cross-laminated sandstone (Whale rock, sol 796) in the Pahrump area, Gale crater. (f) Conglomerate Link (sol 27) near the Bradbury landing site of the Curiosity rover, Gale crater. Supplemental Online Material (SOM) Figures 1 and 2 provide context images (with wider field of view) for Figures 1e and 1f, respectively. Flow directions indicated by arrow in (a–d). North is up in images (a–d). Credit: NASA/JPL/MSSS. Image (e) presents a view towards SSE (~160°). However, there is uncertainty if the imaged sediment block is still in place, or has been rotated since deposition. Hence flow direction cannot be inferred from that image in an absolute sense.

Figure 1

Fig. 2. NASA’s landed missions with timeframes of operations on the surface of Mars. These missions served primarily geology/geochemistry, mineralogy or biology (labeled, respectively, by “geo”, “min” and “biology”). (a) Model of the Viking landers in Death Valley, California, USA (Carl Sagan, 1934–1996). SOM-Figure 3 shows a view of the Martian landscape acquired by Viking Lander 2 including its aluminum biobarrier. (b) Phoenix Mars Lander during assembly. Also shown the Phoenix biobarrier in open and closed state (made of tedlar or [CH2-CHF]n, gas-tight cover of the critical robotic arm). (c) The family of Mars rovers in JPL’s Mars Yard. Credit: NASA/JPL.

Figure 2

Table 1. Pyrolysis and biology experiments onboard the Viking Landers

Figure 3

Fig. 3. Current design of the ExoMars rover (as of January 2016). Credit: ESA. http://exploration.esa.int/mars/51499-exomars-rover/ (accessed January 19, 2016).

Figure 4

Table 2. Science Payload for the ExoMars rover mission, consisting of the solar-powered rover (ESA) and lander platform (Roscosmos). Most instruments listed are mounted to the body, mast or drill of the rover; the lowermost row provides an abbreviated list of instruments onboard the lander platform. The goal of this table is to illustrate the synergy of different payload elements. The instruments within the Analytical Laboratory Drawer (ALD) of the rover body (MicrOmega, RLS, MOMA) can only analyze powdered samples derived from the drill and delivered by the rover's Sample Processing and Distribution System (SPDS). MicrOmega can characterize the mineralogy of the sample as well as detect some organic compounds (provided the latter are exposed on grain surfaces and have absorption bands in the NIR region, i.e. at λ ≤ 3.7 µm). MicrOmega's large field of view (FOV) (5 × 5 mm2) provides the context for ‘point’ measurements by RLS (~0.05 mm) and MOMA (~0.3 mm). MOMA's operational modes are listed (further details in Table 3)

Figure 5

Table 3. MOMA operational modes: pyrolysis, derivatization/thermochemolysis and LDI. The derivatization agents (DAs) are: MTBSTFA/DMF (N-tert-butyldimethylsilyl-N-methyltrifluoroacetamide/dimethylformamide as a 3 : 1 mixture), DMF-DMA (N,N-dimethylformamide-dimethylacetal) or TMAH (25 wt% tetramethylammonium hydroxide in methanol). The compounds given in square brackets behind the DA are the targeted classes of organic compounds in the sample that will be volatilized by chemical reaction with that specific DA in order to be analysed by the GC–MS part of MOMA. The UV laser needed for LDI mode has a power density of (up to) 5 × 1011 W m−2 per pulse. This power density is at least 20 times smaller than the one used for Laser Induced Breakdown Spectroscopy applied by the ChemCam instrument onboard the Curiosity rover (Maurice et al. 2012)

Figure 6

Fig. 4. Overview of the MOMA instrument (Goetz et al.2011). The inclined thick solid line (drawn in blue-green color) represents the laser beam that hits the sample in the refillable sample container at 45°.

Supplementary material: File

Goetz supplementary material

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