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Concepts for the design of an antimatter annihilation rocketMatter-antimatter annihilation is considered for spacecraft propulsion. Annihilation produces considerably more energy per unit mass of propellant than any other known means of energy production. An antimatter annihilation rocket requires several systems and components that are unique to its nature. Among these are an antimatter storage system, a means to extract the antimatter from storage, a system to transport the antimatter to the rocket engine, and the engine wherein annihilation occurs and thrust is produced. Design concepts of these systems and components are presented and discussed.
Document ID
19820013176
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Morgan, D. L., Jr.
(Morgan (David L., Jr.) Livermore, CA, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1982
Subject Category
Nuclear And High-Energy Physics
Report/Patent Number
NAS 1.26:168660
NASA-CR-168660
Accession Number
82N21050
Funding Number(s)
CONTRACT_GRANT: NASA ORDER LH-739408
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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