The Plasma Core Reactor

reportActive / Technical Report | Accesssion Number: AD0258979 | Open PDF

Abstract:

Two types of plasma core reactor, considered as a space propulsion system of thrust-to-weight ratio exceeding unity, are investigated; viz, the simple magnetic bottle and the homopolar configurations. The principal system variables are indicated, and some upper- and lower-bounds for these are derived. The major problem areas and difficulties affecting feasibility are discussed.

Author(s):
Nelson, Seymour T.
Author Organization(s):
AEROSPACE CORP EL SEGUNDO CA
Funding Organization(s):
Air Force Ballistic Missile Division, Inglewood , CA
Document Type:
Technical Report/Technical Report
Publication Date:
1961 May 10
Pagination:
124

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution Code:
A - Approved For Public Release
Distribution Statement: Public Release

RECORD

Collection: TRECMS
Identifying Numbers
Contract Number(s):
AF 04(647)-594
Subject Terms
Modernization Areas:
Hypersonics
Communities of Interest:
Energy and Power Technologies
Descriptor(s):
nuclear energy, magnetic fields, thermal neutrons, electromagnetic fields, propulsion systems, energy transfer, heat energy, heat transfer, magnetic mirrors, nuclear properties, nuclear reactors, particles, boundary layer, electric fields, energy, fissionable materials, high acceleration
Subject Categories:
Propulsion, Engines and Fuels; Nuclear Science and Technology
Update Date:
2022 Apr 26