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Interplanetary propulsion using inertial fusionInertial fusion can be used to power spacecraft within the solar system and beyond. Such spacecraft have the potential for short-duration manned-mission performance exceeding other technologies. We are conducting a study to assess the systems aspects of inertial fusion as applied to such missions, based on the conceptual engine design of Hyde (1983) we describe the required systems for an entirely new spacecraft design called VISTA that is based on the use of DT fuel. We give preliminary design details for the power conversion and power conditioning systems for manned missions to Mars of total duration of about 100 days. Specific mission performance results will be published elsewhere, after the study has been completed.
Document ID
19880003158
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Orth, C. D.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Hogan, W. J.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Hoffman, N.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Murray, K.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Klein, G.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Diaz, F. C.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1987
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
UCRL-95275-REV-1
NAS 1.15:89661
DE87-014342
NASA-TM-89661
CONF-870102-29-REV-1
Report Number: UCRL-95275-REV-1
Report Number: NAS 1.15:89661
Report Number: DE87-014342
Report Number: NASA-TM-89661
Report Number: CONF-870102-29-REV-1
Accession Number
88N12540
Funding Number(s)
CONTRACT_GRANT: W-7405-ENG-48
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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