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Power generation technology options for a Mars missionThe power requirements and resultant power system performances of an aggressive Mars mission are characterized. The power system technologies discussed will support both cargo and piloted space transport vehicles as well as a six-person crew on the Martian surface for 600 days. The mission uses materials transported by cargo vehicles and materials produced using in-situ planetary feed stock to establish a life-support cache and infrastructure for the follow-on piloted lander. Numerous power system technical options are sized to meet the mission power requirements using conventional and solar, nuclear, and wireless power transmission technologies for stationary, mobile surface, and space applications. Technology selections will depend on key criteria such as mass, volume, area, maturity, and application flexibility.
Document ID
19940020208
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bozek, John M.
(NASA Lewis Research Center Cleveland, OH, United States)
Cataldo, Robert L.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1994
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
E-8310
NAS 1.15:106451
NASA-TM-106451
Report Number: E-8310
Report Number: NAS 1.15:106451
Report Number: NASA-TM-106451
Meeting Information
Meeting: Symposia on Space Nuclear Power Systems
Location: Albuquerque, NM
Country: United States
Start Date: January 9, 1994
End Date: January 13, 1994
Sponsors: University of New Mexico
Accession Number
94N24681
Funding Number(s)
PROJECT: RTOP 233-02-0B
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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