DocumentCode :
152355
Title :
A new rocketsonde for upper-air atmospheric measurements
Author :
Newkirk, M.H. ; Hanley, T.R. ; Slujtner, F.J.
Author_Institution :
Appl. Phys. Lab., Johns Hopkins Univ., Laurel, MD, USA
fYear :
2014
fDate :
6-11 July 2014
Firstpage :
231
Lastpage :
231
Abstract :
Summary form only given: The Johns Hopkins University Applied Physics Laboratory (JHU/APL) has developed a new rocket-launched rawinsonde system that measures traditional parameters including temperature, relative humidity, atmospheric pressure, and GPS position. This new “rocketsonde” system was designed specifically for the purpose of deriving vertical profiles of modified refractivity and wind conditions within the lower several thousand meters of the atmosphere.The system is similar to one that was commercially available up until the mid-2000´s, but with additional capabilities not possible with the older system, including use of open-source hardware and software, additional analog and digital channels, improved two-way communications and GPS. It was designed to integrate with the existing JHU/APL Automated Environmental Assessment System (AEAS) that has been used for numerous test events since 2004. The AEAS provides continuous shipboard measurements in the marine layer to characterize the evaporation duct, while the rocketsonde provides upper-air measurements to characterize subrefraction, surface ducting and elevated ducting, if present. In this way the data from both the existing AEAS hardware and the new rocketsonde system can be used to provide a complete assessment of the refractive environment for use in radio frequency (RF) propagation models, which in turn is used in RF system performance models. The rocketsonde allows for easier deployment than balloon-borne sensors in high winds and is faster to deploy. Since the data are collected on descent, the rocketsonde also provides more accurate measurements in the surface layer, away from the effects of the ship´s air wake - which can be significant for larger vessels. Additionally, the rocketsonde sensor package weighs approximately one quarter as much as a typical radiosonde, making it a more viable payload for a UAV. This presentation will provide an overview of the new rocketsonde syst- m and comparisons with commercially available radiosondes and other JHU/APL-developed sensors, including the Helicopter Atmospheric Profiling System (HAPS).
Keywords :
atmospheric techniques; radiosondes; radiotelemetry; sensor placement; AEAS; GPS position measurement; HAPS; JHU/APL-developed sensor; Johns Hopkins university applied physics laboratory; RF system performance model; UAV; analog channel; atmospheric pressure measurement; automated environmental assessment system; balloon-borne sensor; digital channel; elevated ducting; evaporation duct; helicopter atmospheric profiling system; marine layer; open-source hardware; open-source software; radio frequency propagation model; radiosonde; refractivity; relative humidity measurement; rocket-launched rawinsonde system; rocketsonde sensor package; rocketsonde system; shipboard measurement; subrefraction characterization; surface ducting; temperature measurement; two-way communication; unmanned aerial vehicle; upper-air atmospheric measurement; wind condition; Atmospheric measurements; Educational institutions; Global Positioning System; Laboratories; Physics; Sensors; Temperature measurement;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Radio Science Meeting (Joint with AP-S Symposium), 2014 USNC-URSI
Conference_Location :
Memphis, TN
Type :
conf
DOI :
10.1109/USNC-URSI.2014.6955614
Filename :
6955614
Link To Document :
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