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Design of a large aperture Space-based Proton and Electron Energy Detector as payload of IITMSAT
Date Issued
29-09-2015
Author(s)
Shankar, Athreya
Yalamarthy, Ananth Saran
Shah, Tirth
Kelkar, Varun
Mallampalli, Abhishikth
Vikram, A. Amit
Ravindran, Rewanth
Indian Institute of Technology, Madras
Indian Institute of Technology, Madras
Abstract
IITMSAT is a student satellite being developed with a mission to measure charged particle energies and fluxes, and to study the precipitation of these particles from the Van Allen radiation belts. The Space-based Proton Electron Energy Detector (SPEED) is the payload detector aboard IITMSAT which is designed to carry out the mission of charge particle detection and energy measurement in low earth orbit (LEO). This paper details the design of the detector that meets the challenging requirements posed by the mission.
Volume
2015-September