Director of Research (if dissertation) or Advisor (if thesis)
Lembeck, Michael F
Department of Study
Aerospace Engineering
Discipline
Aerospace Engineering
Degree Granting Institution
University of Illinois at Urbana-Champaign
Degree Name
M.S.
Degree Level
Thesis
Keyword(s)
CubeSat
de-orbit
deorbit
de-orbit technology
deorbit technology
space debris
space debris removal
space debris mitigation
LEO
Abstract
The Federal Communications Commission has recently adopted a Low Earth Orbit spacecraft disposal time requirement of five years following mission completion. CubeSats and nanosatellites allow increased access to space for smaller organizations and educational institutions, have lifetimes of up to 25 years in high orbits, but usually have no de-orbit capability. Preventative and removal technologies are essential for addressing this growing problem of inactive satellites remaining in orbit after their mission is completed. Preliminary design of the Next Era Individualized Geo-conscious High Body Orbit Remediator (NEIGHBOR) is assessed for its feasibility in curbing the risk that small satellites pose to the increasingly problematic space debris environment.
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