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

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Lunar L<strong>and</strong>er Network⎯Four L<strong>and</strong>ers<br />

SOURCE: NASA Mission Study (transmitted from George J. Tahu, NASA<br />

<strong>Planetary</strong> <strong>Science</strong> Division)<br />

Scientific Objectives<br />

• Enhance knowledge of lunar <strong>in</strong>terior<br />

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

– Determ<strong>in</strong>e lateral variations <strong>in</strong> <strong>the</strong> structure <strong>and</strong><br />

composition of <strong>the</strong> lunar crust, upper mantle, lower<br />

mantle, <strong>and</strong> lunar core<br />

– Determ<strong>in</strong>e distribution <strong>and</strong> orig<strong>in</strong> of lunar seismic<br />

activity<br />

– Determ<strong>in</strong>e <strong>the</strong> lunar global heat flow budget to better<br />

constra<strong>in</strong> knowledge of lunar <strong>the</strong>rmal evolution<br />

– Determ<strong>in</strong>e bulk lunar composition of radioactive heat‐<br />

produc<strong>in</strong>g elements<br />

– Determ<strong>in</strong>e nature <strong>and</strong> orig<strong>in</strong> of lunar crustal magnetic<br />

field<br />

Key Parameters<br />

• Payload<br />

– Seismometer<br />

– Heat Flow Experiment<br />

– Electromagnetic Sounder<br />

– Lunar Laser Rang<strong>in</strong>g<br />

– Guest Payload<br />

– Education/Public Outreach Pancam<br />

• Advanced Stirl<strong>in</strong>g Radioisotope Generator Surface Power<br />

• Launch Mass: 3572 kg (257 kg <strong>in</strong>dividual l<strong>and</strong>er mass)<br />

• Launch Date: 2016 (on Atlas V 511)<br />

• Direct lunar near‐side l<strong>and</strong><strong>in</strong>g<br />

Lunar Geophysical Network<br />

Key Challenges<br />

• DACS Propulsion<br />

– Development needed <strong>for</strong> MON‐25/MMH combustion<br />

stability<br />

• Mass<br />

– Low dry mass cont<strong>in</strong>gency <strong>for</strong> this development phase<br />

– Propulsion requirements multiply impact to overall mass<br />

growth<br />

• Reliability<br />

– S<strong>in</strong>gle‐str<strong>in</strong>g network reliability<br />

• Mission Operations<br />

– High tempo operations <strong>for</strong> multi‐l<strong>and</strong>er cruise <strong>and</strong><br />

l<strong>and</strong><strong>in</strong>g phase<br />

Key Cost Element Comparison<br />

Cost Risk Analysis S‐Curve<br />

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

C-9

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