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Vision and Voyages for Planetary Science in the - Solar System ...

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Cach<strong>in</strong>g Mars Rover<br />

SOURCE: NASA Mission Study (transmitted from Lisa May, NASA <strong>Planetary</strong> <strong>Science</strong><br />

Division)<br />

Scientific Objectives<br />

• Per<strong>for</strong>m <strong>in</strong> situ science on Mars samples to look <strong>for</strong><br />

evidence of ancient life or pre‐biotic chemistry<br />

• Collect, document, <strong>and</strong> package samples <strong>for</strong> future<br />

collection <strong>and</strong> return to Earth<br />

• Key science <strong>the</strong>mes:<br />

– The search <strong>for</strong> extant life on Mars<br />

– The search <strong>for</strong> evidence of past life on Mars<br />

– Underst<strong>and</strong><strong>in</strong>g martian climate history<br />

– Determ<strong>in</strong>ation of <strong>the</strong> ages of geologic terra<strong>in</strong>s on Mars<br />

– Underst<strong>and</strong><strong>in</strong>g surface‐atmosphere <strong>in</strong>teractions on<br />

Mars<br />

– Underst<strong>and</strong><strong>in</strong>g martian <strong>in</strong>terior processes<br />

Key Parameters<br />

• Model Payload With Sampl<strong>in</strong>g/Cach<strong>in</strong>g <strong>System</strong><br />

– Pancam high resolution stereo imager (on mast)<br />

– Near‐Infrared Po<strong>in</strong>t Spectrometer<br />

– Microscopic Imager<br />

– Alpha‐Particle X‐ray Spectrometer<br />

– Dual Wavelength Raman/Fluorescence Instrument<br />

– Sample H<strong>and</strong>l<strong>in</strong>g, Encapsulation, <strong>and</strong> Conta<strong>in</strong>erization<br />

(arm, corer/abrader, organic blank, h<strong>and</strong>l<strong>in</strong>g <strong>and</strong><br />

conta<strong>in</strong>er system)<br />

• Two x 2.2 m diameter Ultraflex solar arrays<br />

• Launch Mass: 4457 kg<br />

• Launch Date: 2018 (on Atlas V 531)<br />

• Orbit: Type I transfer direct to Mars surface<br />

– 15° S to 25° N latitude<br />

Mars Astrobiology Explorer‐Cacher<br />

Key Challenges<br />

• Vehicle Capabilities Beyond Mars <strong>Science</strong> Laboratory<br />

– Terra<strong>in</strong>‐relative descent navigation <strong>and</strong> precision<br />

l<strong>and</strong><strong>in</strong>g with pallet<br />

– Aeroshell volume to accommodate MAX‐C, ExoMars,<br />

<strong>and</strong> pallet<br />

– Increased rover traverse speed over MSL <strong>and</strong> MER<br />

• Sample H<strong>and</strong>l<strong>in</strong>g, Encapsulation, <strong>and</strong> Conta<strong>in</strong>erization<br />

(SHEC)<br />

– Lack of maturity <strong>in</strong> SHEC subsystem<br />

– Affect of planetary protection <strong>and</strong> sample transfer<br />

requirements<br />

• Mass<br />

– Insufficient mass growth cont<strong>in</strong>gency <strong>for</strong> this<br />

development phase<br />

– Low launch marg<strong>in</strong> <strong>for</strong> this development phase<br />

Key Cost Element Comparison<br />

Cost Risk Analysis S‐Curve<br />

PREPUBLICATION COPY—SUBJECT TO FURTHER EDITORIAL CORRECTION<br />

C-10

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