Computer Science – Performance
Scientific paper
Sep 1979
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1979muni.iafcr....n&link_type=abstract
International Astronautical Federation, International Astronautical Congress, 30th, Munich, West Germany, Sept. 17-22, 1979, 15
Computer Science
Performance
Flight Mechanics, Mars (Planet), Mission Planning, Performance Prediction, Remotely Piloted Vehicles, Flight Characteristics, Graphs (Charts), Space Exploration, Tables (Data), Technology Assessment, User Requirements
Scientific paper
Exploration of Mars by vehicles in Martian atmosphere is considered by a small remotely piloted vehicle launched by the European launcher Ariane. The Martian surface to be explored by the projected Mars Reconnaissance Aircraft (MRA), its design requirements related to environmental factors, and the proposed design to provide a minimum induced drag are discussed. The proposed propulsion systems using electric motors or piston engines propelled by hydrazine monopropellant fuel are described, showing their range vs. payload. The mission profile is compared to NASA Mini-Sniffer and the JPL Mars Flyer, noting that the MRA-100 is superior in range to Mini-Sniffer. It is concluded that Mars reconnaissance aircraft is feasible from flight mechanics standpoint, but transport to Mars remains a problem.
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