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TEST: A Modular Scientific Nanosatellite

Authors :
A. Kirchoff
Art White
J. Dailey
J. Hibbs
M. Maple
J. J. Zapf
David L. Voss
D. P. Hagerman
Hank D. Voss
Farzad Kamalabadi
Source :
Space 2004 Conference and Exhibit.
Publication Year :
2004
Publisher :
American Institute of Aeronautics and Astronautics, 2004.

Abstract

A powerfully instrumented, reliable, low -cost, and 3 -axis stabilized nanosatellite is being developed as part of the Air Force University Nanosatellite -3 Program. The Thunderstorm Effects in Space: Technology (TEST) nanosatellite imple ments a new, highly modular satellite bus structure and common electrical interface that is conducive to satellite modeling, development, testing, and integration flow. TEST is a low -cost ($0.2 M) nanosatellite (30kg) in final development by Taylor Univer sity and the University of Illinois. TEST implements a variety of plasma, energetic particle, and remote sensing instrumentation with the objective of understanding how lightning and thunderstorms influence the upper atmosphere and the near -space environme nt. The TEST modular design and instrumentation challenges portions of satellite systems (such as future DOD DMSP and NASA LWS Geospace Missions), while complementing large multi -probe and remote sensing programs. TEST includes a variety of proven instrume ntation: two 1m Electric Field (EP) probes, a thermal plasma density Langmuir Probe (LP), a 5 to 100 kHz Very Low Frequency (VLF) Receiver, two large geometric factor cooled ( -60 ° C) Solid State Detector (SSD) spectrometers for energetic electrons and ions (10 keV< E

Details

Database :
OpenAIRE
Journal :
Space 2004 Conference and Exhibit
Accession number :
edsair.doi...........1b96bc9483eb6c1bc24504ef91639b84
Full Text :
https://doi.org/10.2514/6.2004-6121