The maximum permissible load on the frontal surface of vehicles, which implement aerodynamic descent in the atmosphere of Mars

Details The maximum permissible load on the frontal surface of vehicles, which implement aerodynamic descent in the atmosphere of Mars The maximum permissible load on the frontal surface of vehicles, which implement aerodynamic descent in the atmosphere of Mars

Feb 1975

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1975stin...7533147i&link_type=abstract

The maximum permissible load on the frontal surface of vehicles, which implement aerodynamic descent in the atmosphere of Mars

Physics

Aerodynamic Loads, Descent Trajectories, Mars Atmosphere, Mars Landing, Atmospheric Entry, Autonomous Navigation, Lift Drag Ratio, Mars Probes, Navigation Aids, Soft Landing

Scientific paper

The descent of ballistic type vehicles into the rarefied atmosphere of
Mars is examined in terms of the effect of aerodynamic loads on the
frontal surface of vehicles. It is shown that a soft landing is feasible
only under the following conditions: presence of autonomous navigation
aids on-board the vehicle, and a small lift-to-drag ratio.

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