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Exobiology in the Solar System & The Search for Life on Mars - ESA

Exobiology in the Solar System & The Search for Life on Mars - ESA

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SP-1231<br />

142<br />

atures should be per<str<strong>on</strong>g>for</str<strong>on</strong>g>med: at least <strong>on</strong>e dur<str<strong>on</strong>g>in</str<strong>on</strong>g>g <str<strong>on</strong>g>the</str<strong>on</strong>g> lowest temperature period (night)<br />

and <strong>on</strong>e dur<str<strong>on</strong>g>in</str<strong>on</strong>g>g <str<strong>on</strong>g>the</str<strong>on</strong>g> highest temperature period (day).<br />

To acquire <strong>on</strong>e spectrum will take approximately 8-12 h depend<str<strong>on</strong>g>in</str<strong>on</strong>g>g <strong>on</strong> <str<strong>on</strong>g>the</str<strong>on</strong>g> phases<br />

and <str<strong>on</strong>g>the</str<strong>on</strong>g> total ir<strong>on</strong> c<strong>on</strong>tent. <str<strong>on</strong>g>The</str<strong>on</strong>g> temperature variati<strong>on</strong> <str<strong>on</strong>g>for</str<strong>on</strong>g> <strong>on</strong>e spectrum should be not<br />

larger than about 10ºC. In case of larger variati<strong>on</strong>s, spectra <str<strong>on</strong>g>for</str<strong>on</strong>g> different temperature<br />

ranges will be stored separately, result<str<strong>on</strong>g>in</str<strong>on</strong>g>g <str<strong>on</strong>g>in</str<strong>on</strong>g> an <str<strong>on</strong>g>in</str<strong>on</strong>g>creased total measur<str<strong>on</strong>g>in</str<strong>on</strong>g>g time<br />

(depend<str<strong>on</strong>g>in</str<strong>on</strong>g>g <strong>on</strong> <str<strong>on</strong>g>the</str<strong>on</strong>g> number of temperature <str<strong>on</strong>g>in</str<strong>on</strong>g>tervals required).<br />

<str<strong>on</strong>g>The</str<strong>on</strong>g> MIMOS II <str<strong>on</strong>g>in</str<strong>on</strong>g>strument developed at <str<strong>on</strong>g>the</str<strong>on</strong>g> Technische Universität Darmstadt,<br />

Germany, was scheduled to fly <strong>on</strong> Russia’s <strong>Mars</strong>-98 rover missi<strong>on</strong>. This <str<strong>on</strong>g>in</str<strong>on</strong>g>strument<br />

has been developed and a prototype built and partially qualified <str<strong>on</strong>g>for</str<strong>on</strong>g> <str<strong>on</strong>g>the</str<strong>on</strong>g> Russian-<br />

German Nanokhod <str<strong>on</strong>g>in</str<strong>on</strong>g>strument deployment device (IDD; Max-Planck Institute <str<strong>on</strong>g>for</str<strong>on</strong>g><br />

Cosmochemistry, Ma<str<strong>on</strong>g>in</str<strong>on</strong>g>z, Germany), which was scheduled to fly <strong>on</strong> Europe’s Inter-<br />

<strong>Mars</strong>Net missi<strong>on</strong>. A MIMOS II prototype was successfully tested <strong>on</strong> <str<strong>on</strong>g>the</str<strong>on</strong>g> Rocky-7<br />

prototype rover dur<str<strong>on</strong>g>in</str<strong>on</strong>g>g <str<strong>on</strong>g>the</str<strong>on</strong>g> May 1997 field tests <str<strong>on</strong>g>in</str<strong>on</strong>g> <str<strong>on</strong>g>the</str<strong>on</strong>g> US Mojave Desert, tak<str<strong>on</strong>g>in</str<strong>on</strong>g>g data<br />

under semi-real c<strong>on</strong>diti<strong>on</strong>s.<br />

<str<strong>on</strong>g>The</str<strong>on</strong>g> Mössbauer spectrometer is a simple <str<strong>on</strong>g>in</str<strong>on</strong>g>strument. <str<strong>on</strong>g>The</str<strong>on</strong>g> ma<str<strong>on</strong>g>in</str<strong>on</strong>g> parts are <str<strong>on</strong>g>the</str<strong>on</strong>g><br />

radiati<strong>on</strong> source, <str<strong>on</strong>g>the</str<strong>on</strong>g> velocity transducer (drive), <str<strong>on</strong>g>the</str<strong>on</strong>g> Silic<strong>on</strong> PIN (positive-<str<strong>on</strong>g>in</str<strong>on</strong>g>tr<str<strong>on</strong>g>in</str<strong>on</strong>g>sicnegative)<br />

radiati<strong>on</strong> detectors and <str<strong>on</strong>g>the</str<strong>on</strong>g>ir pre- and ma<str<strong>on</strong>g>in</str<strong>on</strong>g>-amplifiers, and <str<strong>on</strong>g>the</str<strong>on</strong>g> <str<strong>on</strong>g>in</str<strong>on</strong>g>strument<br />

c<strong>on</strong>trol and data acquisiti<strong>on</strong> system.<br />

<str<strong>on</strong>g>The</str<strong>on</strong>g> standard 57 Co radiati<strong>on</strong> source is used, embedded <str<strong>on</strong>g>in</str<strong>on</strong>g> a solid rhodium matrix,<br />

which is mounted <str<strong>on</strong>g>in</str<strong>on</strong>g> a titanium holder. This design is <str<strong>on</strong>g>in</str<strong>on</strong>g>tr<str<strong>on</strong>g>in</str<strong>on</strong>g>sically simple, rugged and<br />

is made very safe through <str<strong>on</strong>g>the</str<strong>on</strong>g> shield<str<strong>on</strong>g>in</str<strong>on</strong>g>g design. <str<strong>on</strong>g>The</str<strong>on</strong>g> drive is a unique m<str<strong>on</strong>g>in</str<strong>on</strong>g>iature<br />

double-voice coil electromechanical drive, developed at TU Darmstadt. <str<strong>on</strong>g>The</str<strong>on</strong>g> drive<br />

system has already underg<strong>on</strong>e envir<strong>on</strong>mental test<str<strong>on</strong>g>in</str<strong>on</strong>g>g at +20ºC to -80ºC, as well as<br />

vibrati<strong>on</strong> and shock tests <str<strong>on</strong>g>in</str<strong>on</strong>g> <str<strong>on</strong>g>the</str<strong>on</strong>g> frequency range specified <str<strong>on</strong>g>for</str<strong>on</strong>g> <str<strong>on</strong>g>the</str<strong>on</strong>g> Russian <strong>Mars</strong>-98<br />

lander missi<strong>on</strong>. <str<strong>on</strong>g>The</str<strong>on</strong>g> Si-PIN-diodes toge<str<strong>on</strong>g>the</str<strong>on</strong>g>r with <str<strong>on</strong>g>the</str<strong>on</strong>g> pre- and ma<str<strong>on</strong>g>in</str<strong>on</strong>g>-amplifiers and <str<strong>on</strong>g>the</str<strong>on</strong>g><br />

bias supply have been tested <str<strong>on</strong>g>in</str<strong>on</strong>g> <str<strong>on</strong>g>the</str<strong>on</strong>g> same way (shock, frequency, temperature).<br />

Prototype versi<strong>on</strong>s operated successfully at even unfavourably high temperatures<br />

dur<str<strong>on</strong>g>in</str<strong>on</strong>g>g <str<strong>on</strong>g>the</str<strong>on</strong>g> Rocky-7 field tests. <str<strong>on</strong>g>The</str<strong>on</strong>g> <str<strong>on</strong>g>in</str<strong>on</strong>g>strument c<strong>on</strong>trol unit and data acquisiti<strong>on</strong><br />

system, <str<strong>on</strong>g>in</str<strong>on</strong>g>clud<str<strong>on</strong>g>in</str<strong>on</strong>g>g <str<strong>on</strong>g>the</str<strong>on</strong>g> software, successfully operated <str<strong>on</strong>g>in</str<strong>on</strong>g> a number of laboratory<br />

measurements as well as <str<strong>on</strong>g>the</str<strong>on</strong>g> Rocky-7 field tests <str<strong>on</strong>g>in</str<strong>on</strong>g> May 1997. For <str<strong>on</strong>g>the</str<strong>on</strong>g> <strong>Mars</strong> Surveyor<br />

2001 A<str<strong>on</strong>g>the</str<strong>on</strong>g>na missi<strong>on</strong>, <str<strong>on</strong>g>the</str<strong>on</strong>g> MIMOS II <str<strong>on</strong>g>in</str<strong>on</strong>g>strument will be split <str<strong>on</strong>g>in</str<strong>on</strong>g>to two parts: a detector<br />

head mounted <strong>on</strong> <str<strong>on</strong>g>the</str<strong>on</strong>g> arm, and <str<strong>on</strong>g>the</str<strong>on</strong>g> <str<strong>on</strong>g>in</str<strong>on</strong>g>strument c<strong>on</strong>trol and data acquisiti<strong>on</strong> unit located<br />

<str<strong>on</strong>g>in</str<strong>on</strong>g> <str<strong>on</strong>g>the</str<strong>on</strong>g> Rover’s warm electr<strong>on</strong>ics box.<br />

<str<strong>on</strong>g>The</str<strong>on</strong>g> total weight is about 500 g, with <str<strong>on</strong>g>the</str<strong>on</strong>g> sensor head itself about 400 g. <str<strong>on</strong>g>The</str<strong>on</strong>g> power<br />

c<strong>on</strong>sumpti<strong>on</strong> is of <str<strong>on</strong>g>the</str<strong>on</strong>g> order of 1.5 W. <str<strong>on</strong>g>The</str<strong>on</strong>g> radioactive Mössbauer source will have an<br />

<str<strong>on</strong>g>in</str<strong>on</strong>g>tensity of about 300 mCi at launch.<br />

II.5.7.5 I<strong>on</strong>/Electr<strong>on</strong> Probes, X-ray Spectroscopy<br />

For chemical compositi<strong>on</strong>, <str<strong>on</strong>g>the</str<strong>on</strong>g> i<strong>on</strong> probe is heavy and an alternative could be electr<strong>on</strong><br />

probe analysis. In<str<strong>on</strong>g>for</str<strong>on</strong>g>mati<strong>on</strong> <strong>on</strong> crystal structure could be provided by X-ray<br />

spectroscopy, if m<str<strong>on</strong>g>in</str<strong>on</strong>g>iaturised <str<strong>on</strong>g>for</str<strong>on</strong>g> applicati<strong>on</strong> to planetary explorati<strong>on</strong> missi<strong>on</strong>s. <str<strong>on</strong>g>The</str<strong>on</strong>g>re<br />

are two US teams from <str<strong>on</strong>g>the</str<strong>on</strong>g> NASA Ames Research Center and Los Alamos Nati<strong>on</strong>al<br />

Laboratory work<str<strong>on</strong>g>in</str<strong>on</strong>g>g <strong>on</strong> <str<strong>on</strong>g>the</str<strong>on</strong>g> m<str<strong>on</strong>g>in</str<strong>on</strong>g>iaturisati<strong>on</strong> of X-ray diffracti<strong>on</strong> <str<strong>on</strong>g>in</str<strong>on</strong>g>struments (XRDs).<br />

<str<strong>on</strong>g>The</str<strong>on</strong>g>re are no prototypes available yet. <str<strong>on</strong>g>The</str<strong>on</strong>g> development of flight <str<strong>on</strong>g>in</str<strong>on</strong>g>struments will<br />

require at least 2 years, if successful at all.<br />

II.5.7.6 IR Spectroscopy<br />

II.5.7.6.1 Molecular Spectroscopy<br />

IR spectroscopy at 0.8-4.0 µm can determ<str<strong>on</strong>g>in</str<strong>on</strong>g>e <str<strong>on</strong>g>the</str<strong>on</strong>g> abundances of many types of m<str<strong>on</strong>g>in</str<strong>on</strong>g>erals,<br />

<str<strong>on</strong>g>in</str<strong>on</strong>g>clud<str<strong>on</strong>g>in</str<strong>on</strong>g>g clays, hydrates, and carb<strong>on</strong>ates. Carb<strong>on</strong>ate materials such as magnesite,<br />

calcite and siderite can easily be dist<str<strong>on</strong>g>in</str<strong>on</strong>g>guished from <strong>on</strong>e ano<str<strong>on</strong>g>the</str<strong>on</strong>g>r. All have near-<br />

-<br />

IR features <str<strong>on</strong>g>in</str<strong>on</strong>g> <str<strong>on</strong>g>the</str<strong>on</strong>g> 1.7-2.5 µm range attributable to <str<strong>on</strong>g>the</str<strong>on</strong>g> CO3 ani<strong>on</strong>. Sulphates such as<br />

gypsum and anhydrite have absorpti<strong>on</strong>s <str<strong>on</strong>g>in</str<strong>on</strong>g> <str<strong>on</strong>g>the</str<strong>on</strong>g> 1.0-1.5 µm and 4.0-4.7 µm ranges.<br />

Ferrous absorpti<strong>on</strong>s of pyroxenes are also evident <str<strong>on</strong>g>in</str<strong>on</strong>g> <str<strong>on</strong>g>the</str<strong>on</strong>g> 1.0-2.0 µm regi<strong>on</strong>. <str<strong>on</strong>g>The</str<strong>on</strong>g> ratio<br />

of <str<strong>on</strong>g>the</str<strong>on</strong>g> 1 µm to 2 µm absorpti<strong>on</strong>s is diagnostic of <str<strong>on</strong>g>the</str<strong>on</strong>g> compositi<strong>on</strong>. Although oliv<str<strong>on</strong>g>in</str<strong>on</strong>g>e<br />

has been found <str<strong>on</strong>g>in</str<strong>on</strong>g> <strong>on</strong>ly <strong>on</strong>e martian meteorite, <str<strong>on</strong>g>the</str<strong>on</strong>g> structure of <str<strong>on</strong>g>the</str<strong>on</strong>g> broad absorpti<strong>on</strong>

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