Am. Harri et al., METEOROLOGICAL OBSERVATIONS ON MARTIAN SURFACE - MET-PACKAGES OF MARS-96 SMALL STATIONS AND PENETRATORS, Planetary and space science, 46(6-7), 1998, pp. 779-793
The scientific objectives of a meterological experiment on the Martian
surface are defined, and the meteorological equipment of the landing
elements of the Mars-96 mission are described with emphasis on the app
licability for re-use in forthcoming Mars missions. The general strate
gy for atmospheric surface observations is discussed. Meteorological s
urface observations are of utmost value in studying the Martian atmosp
here. The climatological cycles and atmospheric circulations, as well
as the boundary layer phenomena can be understood thoroughly only, if
the contribution of in situ surface measurements are amalgamated with
the remote observations. The Mars-96 mission had an ambitious goal of
deploying four versatile payloads at four Northern hemispheric sites.
The observations of pressure, temperature, wind, atmospheric optical t
hickness and humidity, as well as pressure and temperature measurement
s during the atmospheric descent were included in the meteorology expe
riment. Even though the Mars-96 mission was unsuccessful, the objectiv
es and implementation of the meteorology experiment are applicable to
any forth-coming landing mission to Mars. This applies both to a missi
on having a number of observation sites spread all over the surface of
Mars, and to a single lander or rover. The main operational objective
of this meteorological experiment is to provide a regular time series
of the meteorological parameters with accelerated measurement campaig
ns during dawn and dusk. Such a data set would substantially improve o
ur understanding of the atmospheric structure, dynamics, climatologica
l cycles, and the atmosphere-surface interactions. The implementation
of the meteorology instrument features advanced sensor technology and
flexible system design. The application on the Mars-96 landing element
s was, however, severely constrained by the limited power supply. The
usefulness of the system can be substantially enhanced by modest addit
ional resources and with few or no design modifications. (C) 1998 Else
vier Science Ltd. All rights reserved.