DocumentCode
252393
Title
Payload system development for high altitude balloon
Author
Haklin Kimm
Author_Institution
Comput. Sci. Dept., East Stroudsburg Univ., East Stroudsburg, PA, USA
fYear
2014
fDate
13-15 Dec. 2014
Firstpage
730
Lastpage
735
Abstract
A balloonSat weighs up to around 4 kg and soars up to reach altitudes of 100,000 feet or higher using a high altitude balloon with its diameter of 10 to 12 feet mostly, but costs only several hundred dollars. This altitude of the stratosphere provides harsh conditions of tough and significant scientific and engineering challenges. High-altitude balloons can carry small payloads to altitudes higher than 80,000 feet into the stratosphere, in which part of space the conditions and atmosphere are quite similar to those in low-Earth orbit, so as to call it as near-space. In this balloonSat project, the payload systems are developed based upon a cubic satellite, which is equipped with a 16-bit microcontroller; wireless 2.4 GHz modem that transmits signals well to a receiver on the ground consistently upon various cosmic radiation levels in the near-space; the 9-degree sensor that collects and transmits in real time during the whole flight. In the meantime to track the BalloonSat throughout the whole flight so as to recover it safely, the GPS and Automatic Position Reporting System (APRS) are deployed with the balloonSat.
Keywords
Earth orbit; aerospace instrumentation; microcontrollers; 16-bit microcontroller; APRS; GPS; automatic position reporting system; balloonSat project; cosmic radiation levels; cubic satellite; frequency 2.4 GHz; high altitude balloon; low-Earth orbit; payload system development; wireless modem; Batteries; Computers; Magnetometers; Modems; Payloads; Receivers; Terrestrial atmosphere;
fLanguage
English
Publisher
ieee
Conference_Titel
System Integration (SII), 2014 IEEE/SICE International Symposium on
Conference_Location
Tokyo
Print_ISBN
978-1-4799-6942-5
Type
conf
DOI
10.1109/SII.2014.7028129
Filename
7028129
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