Electromagnetic extraction and annihilation of antiprotons for spacecraft propulsion

Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2008.

Bibliographic Details
Main Author: Zayas, Daniel Antonio
Other Authors: Raymond J. Sedwick and James A. Bickford.
Format: Thesis
Language:eng
Published: Massachusetts Institute of Technology 2009
Subjects:
Online Access:http://hdl.handle.net/1721.1/45242
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author Zayas, Daniel Antonio
author2 Raymond J. Sedwick and James A. Bickford.
author_facet Raymond J. Sedwick and James A. Bickford.
Zayas, Daniel Antonio
author_sort Zayas, Daniel Antonio
collection MIT
description Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2008.
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spelling mit-1721.1/452422019-04-10T19:36:39Z Electromagnetic extraction and annihilation of antiprotons for spacecraft propulsion Zayas, Daniel Antonio Raymond J. Sedwick and James A. Bickford. Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Aeronautics and Astronautics. Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2008. Includes bibliographical references (p. 85-87). A novel concept for the extraction and long-term trapping of antiprotons from planetary magnetospheres is developed. The excitation via rotating magnetic field of an electron population within a distributed neutral plasma is shown to produce a large-scale magnetic field approximating a dipole with r-² or slower decay. These shallow field gradients are, in turn, found to suppress the natural tendency of the magnetic dipole field to shield against incident particle fluxes. Particle transport and plasma interaction models are developed and used to compare collection performance against various electrostatic and magnetostatic collection systems. Baseline system architectures are presented, and antiproton collection rates on the order of nanograms per day are estimated, far exceeding current Earth-based production rates. To demonstrate the performance potential of antiproton fuels for spacecraft propulsion, a modified rocket equation with relativistic corrections and variable mass-energy conversion efficiency is derived. Antimatter engines operating via the catalysis of nuclear fission in a fissile material by antiprotons are found to be three to four (3 - 4) times more efficient than traditional proton-antiproton annihilation or "beam-core" engines, and vastly more efficient than conventional chemical and electric propulsion systems. Baseline architectures for various missions are presented. by Daniel Antonio Zayas. S.M. 2009-04-29T17:13:57Z 2009-04-29T17:13:57Z 2008 2008 Thesis http://hdl.handle.net/1721.1/45242 309350315 eng M.I.T. theses are protected by copyright. They may be viewed from this source for any purpose, but reproduction or distribution in any format is prohibited without written permission. See provided URL for inquiries about permission. http://dspace.mit.edu/handle/1721.1/7582 87 p. application/pdf Massachusetts Institute of Technology
spellingShingle Aeronautics and Astronautics.
Zayas, Daniel Antonio
Electromagnetic extraction and annihilation of antiprotons for spacecraft propulsion
title Electromagnetic extraction and annihilation of antiprotons for spacecraft propulsion
title_full Electromagnetic extraction and annihilation of antiprotons for spacecraft propulsion
title_fullStr Electromagnetic extraction and annihilation of antiprotons for spacecraft propulsion
title_full_unstemmed Electromagnetic extraction and annihilation of antiprotons for spacecraft propulsion
title_short Electromagnetic extraction and annihilation of antiprotons for spacecraft propulsion
title_sort electromagnetic extraction and annihilation of antiprotons for spacecraft propulsion
topic Aeronautics and Astronautics.
url http://hdl.handle.net/1721.1/45242
work_keys_str_mv AT zayasdanielantonio electromagneticextractionandannihilationofantiprotonsforspacecraftpropulsion