Published August 1991 | Version v1
Report Restricted

Fusion energy for space missions in the 21st Century

Description

Future space missions were hypothesized and analyzed and the energy source for their accomplishment investigated. The mission included manned Mars, scientific outposts to and robotic sample return missions from the outer planets and asteroids, as well as fly-by and rendezvous mission with the Oort Cloud and the nearest star, Alpha Centauri. Space system parametric requirements and operational features were established. The energy means for accomplishing the High Energy Space Mission were investigated. Potential energy options which could provide the propulsion and electric power system and operational requirements were reviewed and evaluated. Fusion energy was considered to be the preferred option and was analyzed in depth. Candidate fusion fuels were evaluated based upon the energy output and neutron flux. Reactors exhibiting a highly efficient use of magnetic fields for space use while at the same time offering efficient coupling to an exhaust propellant or to a direct energy convertor for efficient electrical production were examined. Near term approaches were identified

Availability note (English)

MF available from INIS under the Report Number; NTIS HC/MF A21; INIS.

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Additional details

Publishing Information

Imprint Pagination
477 p.
Report number
N--92-11783

INIS

Country of Publication
United States
Country of Input or Organization
United States
INIS RN
23041327
Subject category
S70: PLASMA PHYSICS AND FUSION TECHNOLOGY;
Resource subtype / Literary indicator
Numerical Data
Descriptors DEI
EFFICIENCY; ENERGY CONVERSION; FEASIBILITY STUDIES; PROPULSION SYSTEMS; SPACE FLIGHT; SPACE VEHICLES; SPACECRAFT POWER SUPPLIES; THEORETICAL DATA; THERMONUCLEAR REACTORS
Descriptors DEC
CONVERSION; DATA; ELECTRONIC EQUIPMENT; EQUIPMENT; INFORMATION; NUMERICAL DATA; POWER SUPPLIES

Optional Information

Secondary number(s)
NASA-TM--4298; NAS--1.15:4298.