Modeling and simulation of a CubeSat with dual electric propulsion systems
Patel, Ravi D
Loading…
Permalink
https://hdl.handle.net/2142/114022
Description
Title
Modeling and simulation of a CubeSat with dual electric propulsion systems
Author(s)
Patel, Ravi D
Issue Date
2021-12-10
Director of Research (if dissertation) or Advisor (if thesis)
Lembeck, Michael
Department of Study
Aerospace Engineering
Discipline
Aerospace Engineering
Degree Granting Institution
University of Illinois at Urbana-Champaign
Degree Name
M.S.
Degree Level
Thesis
Date of Ingest
2022-04-29T21:47:46Z
Keyword(s)
Engineering
Language
eng
Abstract
The CubeSat mission analysis presented here is related to the Dual-Propulsion Experiment (DUPLEX) CubeSat in development by CUAerospace (CUA), with partners at the University of Illinois at Urbana- Champaign, NearSpace Launch, and NanoRacks. This CubeSat features two novel electric propulsion systems designed for use in CubeSats. This thesis presents the pre-flight technical analysis performed to determine the capabilities and limitations of these new propulsion systems. In this study, the theory behind modeling low thrust trajectories for CubeSats is presented. This theory, implemented in high-fidelity thruster performance simulations, was used to develop and test mission profiles for the DUPLEX mission. The results are being shared with the NASA International Space Station operations personnel to assure safe and compatible operations of DUPLEX after deployment from ISS. Through this investigation, the capabilities and limitations of these two new electric propulsion systems for CubeSats have been determined.
Use this login method if you
don't
have an
@illinois.edu
email address.
(Oops, I do have one)
IDEALS migrated to a new platform on June 23, 2022. If you created
your account prior to this date, you will have to reset your password
using the forgot-password link below.
