Sand and dust issues for the MESUR mission

Details Sand and dust issues for the MESUR mission Sand and dust issues for the MESUR mission

May 1991

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1991sdum.nasa...56w&link_type=abstract

In its Sand and Dust on Mars p 56-57 (SEE N91-27057 18-91)

Computer Science

Ablation, Abrasives, Dust, Dust Storms, Erosion, Heat Shielding, Landing Sites, Mars Atmosphere, Mars Surface, Sands, Solar Arrays, Viking Lander Spacecraft, Blowing, Bow Waves, Corrosion, Deposition, Feasibility, Imaging Techniques, Penetration, Recession, Shock Waves

Scientific paper

The presence of particles in the Martian atmosphere increases the rate of erosion of the heat shield during the entry phase of the MESUR mission. Preliminary analysis has shown that under certain conditions particles will penetrate the bow shock of the entry vehicle, impact and erode the heat shield, above the anticipated rate from the ablation process. Knowledge of the distribution, sizes, and composition of particles suspended in the atmosphere will permit the estimation of the heat shield recession both for a nominal Mars atmosphere and in dust storm conditions. On the surface of Mars, sand and dust can effect the operations and design of the science instruments (i.e., imaging) and lander subsystems (i.e., solar arrays). Distribution and deposition of sand and dust on the planet's surface will dictate the feasibility of using solar arrays as a power source for the lander. Furthermore, the potential abrasive nature of blowing particles must be understood in order to properly select suitable materials for lander structure and any components exposed to the environment. The selection of lander material may also be dictated by corrosive and chemically active properties of particles at a potential landing site. Some key interests concerning sand and dust on the surface and in the atmosphere are summarized in a number of questions that are included.

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