Aerostat for the Mars 1994/1996 mission

Details Aerostat for the Mars 1994/1996 mission Aerostat for the Mars 1994/1996 mission

Nov 1991

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1991esasp.317..301t&link_type=abstract

In ESA, 10th ESA Symposium on European Rocket and Balloon Programmes and Related Research p 301-305 (SEE N92-24589 15-12)

Mathematics

Logic

Airships, Balloon Flight, Descent, Mars Landing, Aerospace Engineering, Mission Planning, Roving Vehicles, Technology Assessment, Tethering

Scientific paper

An original vehicle, the Aerosat, to be used as a means of locomotion, either near the Mars surface during atmospheric flight at a few kilometers altitude, or directly in contact with the ground when the Aerosat will be stabilized by its guiderope, is presented. A general description of the mission is given and concepts for the design of the balloon together with its dimensions and technological aspects are discussed.

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