DocumentCode :
1769911
Title :
Numerical study of lander effects on DREAMS scientific package measurements
Author :
Chiodini, Sebastiano ; Colombatti, G. ; Pertile, M. ; Debei, S.
Author_Institution :
CISAS, Univ. degli Studi di Padova, Padua, Italy
fYear :
2014
fDate :
29-30 May 2014
Firstpage :
433
Lastpage :
438
Abstract :
The DREAMS (Dust characterisation, Risk assessment and Environment Analyser on the Martian Surface) sensor suite is designed to investigate Martian meteorology and atmospheric electric properties at the ExoMars 2016 EDM (Entry, Descent and landing demonstrator Module) landing site. The DREAMS package will provides wind speed and direction measurement by means of MetWind hot-film anemometer and near surface temperature by means of MarsTem resistance thermometer sensor. The aim of this work is to investigate and quantify the flow distortion due to the lander and meteorological mast shape and the temperature perturbation due to the buoyant thermal plume from lander. The results of the thermal and Computational Fluid Dynamics (CFD) of the lander will be presented. Moreover, preliminary design of environmental simulation wind tunnel is presented.
Keywords :
Mars; aerospace instrumentation; anemometers; entry, descent and landing (spacecraft); numerical analysis; planetary surfaces; risk management; thermal pollution; thermometers; CFD; DREAMS scientific package measurements; ExoMars 2016 EDM; MarsTem resistance thermometer sensor; MetWind hot-film anemometer; atmospheric electric properties; buoyant thermal plume; computational fluid dynamics; dust characterisation, risk assessment and environment analyser on the Martian surface sensor; entry, descent and landing demonstrator module landing site; environmental simulation wind tunnel design; flow distortion; lander effects; meteorological mast shape; near surface temperature; numerical study; temperature perturbation; Atmospheric modeling; Computational fluid dynamics; Computational modeling; Mars; Temperature measurement; Thermal pollution; Wind speed; Buoyant Thermal Plume; Computational Fluid Dynamics; Planetary Boundary Layer; Planetary landers;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Metrology for Aerospace (MetroAeroSpace), 2014 IEEE
Conference_Location :
Benevento
Type :
conf
DOI :
10.1109/MetroAeroSpace.2014.6865964
Filename :
6865964
Link To Document :
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