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Presentation 406 - International Planetary Probe Workshop

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We’ve come a long way…<br />

• In 2001, Mars Smart Lander: • In 2010, Mars Science Laboratory:<br />

Mars Science Laboratory<br />

• Launch date in 2005<br />

• Peak heat flux of ~170 W/cm 2 (about 1.4<br />

times greater than Pathfinder), laminar<br />

• Asymmetric aeroshell geometry; much<br />

lighter payload (rover); mission “creep”<br />

quickly resulted; 4.05m diam<br />

• Launch date in December 2011 (originally<br />

scheduled for Sept. 2009)<br />

• Peak heat flux of 226 W/cm 2 , fully<br />

turbulent boundary layer before peak<br />

heating<br />

• Symmetric shape; tiled heatshield; rover<br />

much larger than original design;<br />

instrumented heatshield; 4.5m diam<br />

June 16, 2010 7 th <strong>International</strong> <strong>Planetary</strong> <strong>Probe</strong> <strong>Workshop</strong> (IPPW7) HHH-21

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