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MARS
Though we are not aware of any current opportunites to fly penetrators to Mars, the ESA/UK penetrator system study last year (2010) identified two possible significant penetrator applications :-
An advantage of a Martian deployment is the ability to use the atmosphere to aid descent, which can significantly reduce the total system mass. Also, since impact speed is much higher than soft landers (e.g. 300m/s), the use of the atmosphere as a braking force is much less problematic. A mature study of the feasibility of this technology is yet to be undertaken. An example is the potential effect of the iron oxide in the Martian soil on communications to an orbiter from beneath the surface. This will be dependent on signal attenuation, impact crater morphology, impact site characteristics, and whether an umbilical to the surface could be arranged to e.g. from a descent parachute. Mars Penetrator Presentations
1st February 2011, Rob Gowen. rag@mssl.ucl.ac.uk Mullard Space Science Laboratory - Holmbury St. Mary, Dorking, Surrey. RH5 6NT. - +44 (0)1483 204100 - Copyright © 1999-2005 UCL
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