The Delaware Atmospheric Plasma Probe Experiment: the flight computer and science instrument subsystem

Author(s)Khan, Ranyah
Date Accessioned2025-05-27T18:23:20Z
Date Available2025-05-27T18:23:20Z
Publication Date2025
SWORD Update2025-05-19T01:02:10Z
AbstractThis thesis presents the development and evolution of the Flight Computer and Science Instrument Subsystem for the Delaware Atmospheric Plasma Probe Experiment (DAPPEr), a 3U CubeSat mission designed to study ionospheric plasma. The research details two major iterations of these systems, with the first successfully tested on NASA’s RockSat-C sounding rocket mission in 2024, and the second designed for DAPPEr’s planned launch. The work validates these designs through the successful collection of electron density and temperature measurements in the lower ionosphere during the UDIP-4 mission, where data showed strong agreement with the International Reference Ionosphere model. DAPPEr will expand upon this foundation by deploying dual Langmuir probes at 400-450 km altitude to investigate plasma characteristics and spacecraft charging effects by alternating between grounding to the rocket-skin or the Langmuir probes. As the first spacecraft led by a Delaware team, DAPPEr will act as a stepping stone for Delaware’s space program development, while advancing both the scientific understanding of ionospheric plasma through CubeSat-based measurement techniques.
AdvisorMaruca, Bennett A.
AdvisorKiamilev, Fouad E.
DegreeM.S.
DepartmentUniversity of Delaware, Department of Electrical and Computer Engineering
Unique Identifier1523074478
URLhttps://udspace.udel.edu/handle/19716/36243
Languageen
PublisherUniversity of Delaware
URIhttps://www.proquest.com/pqdtlocal1006271/dissertations-theses/delaware-atmospheric-plasma-probe-experiment/docview/3205346837/sem-2?accountid=10457
KeywordsIonospheric plasma
KeywordsIonosphere model
KeywordsElectron density
KeywordsPlasma
KeywordsSpacecraft
TitleThe Delaware Atmospheric Plasma Probe Experiment: the flight computer and science instrument subsystem
TypeThesis
Files
Original bundle
Now showing 1 - 1 of 1
Loading...
Thumbnail Image
Name:
Khan_udel_0060M_16394.pdf
Size:
7 MB
Format:
Adobe Portable Document Format
License bundle
Now showing 1 - 1 of 1
No Thumbnail Available
Name:
license.txt
Size:
2.22 KB
Format:
Item-specific license agreed upon to submission
Description: