Balloon versus aircraft for research on Mars

Details Balloon versus aircraft for research on Mars Balloon versus aircraft for research on Mars

Feb 1980

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1980stin...8123003r&link_type=abstract

Unknown

Computer Science

Balloons, Light Aircraft, Mars Atmosphere, Mars Environment, Mars Landing, Aerodynamic Drag, Feasibility Analysis, Hydrazine Engines, Planetary Gravitation

Scientific paper

Simple theoretical considerations taking displaced volumes, gas densities, device mass, and gravity into consideration are used to investigate the aptitudes of balloons and aircraft. Although apparently more complex, aircraft operation is shown to be more feasible in the Martian atmosphere. The characteristics of this atmosphere make balloon flight at an altitude of 3 km equivalent to Earth flight at on altitude of 35.7 km. Aircraft flight, however, in the Martian atmosphere at an altitude of 1 km is only equivalent to Earth flight at an altitude of 13.2 km. A hydrazine engine powered aircraft is proposed.

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