The effectiveness of the use of an aerodynamic lift with descent in the atmosphere of Mars

Details The effectiveness of the use of an aerodynamic lift with descent in the atmosphere of Mars The effectiveness of the use of an aerodynamic lift with descent in the atmosphere of Mars

Feb 1975

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1975stin...7530216i&link_type=abstract

The effectiveness of the use of an aerodynamic lift with descent in the atmosphere of Mars Transl. into ENGLISH from Uch. Zap.

Physics

Aerodynamic Coefficients, Descent Trajectories, Lift, Mars Atmosphere, Atmospheric Entry, Equations Of Motion, Lift Drag Ratio, Soft Landing

Scientific paper

Two limiting cases of a reduction in the descent vehicle in the atmosphere of Mars were examined: descent with constant lift-drag ratio, and descent with the optimum control of aerodynamic lift. A numerical analysis is included, and it is shown that it is necessary to evaluate energy expenditures on active braking and by weight of descent control system before a descent method can be chosen.

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