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Mars manned transportation vehicleA viable power system technology for a surface transportation vehicle to explore the planet Mars is presented. A number of power traction systems were investigated, and it was found that a regenerative hydrogen-oxygen fuel cell appears to be attractive for a manned Mars rover application. Mission requirements were obtained from the Manned Mars Mission Working Group. Power systems weights, power, and reactants requirements were determined as a function of vehicle weights for vehicles weighting from 6,000 to 16,000 lb (2,722 to 7,257 kg), (Earth weight). The vehicle performance requirements were: velocity, 10 km/hr; range, 100 km; slope climbing capability, 30 deg uphill for 50 km; mission duration, 5 days; and crew, 5. Power requirements for the operation of scientific equipment and support system capabilities were also specified and included in this study. The concept developed here would also be applicable to a Lunar based vehicle for Lunar exploration. The reduced gravity on the Lunar surface, (over that on the Martian surface), would result in an increased range or capability over that of the Mars vehicle since many of the power and energy requirements for the vehicle are gravity dependent.
Document ID
19900029514
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Perez-Davis, Marla E.
(NASA Lewis Research Center Cleveland, OH, United States)
Faymon, Karl A.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1989
Subject Category
Ground Support Systems And Facilities (Space)
Report/Patent Number
AAS PAPER 87-271
Report Number: AAS PAPER 87-271
Accession Number
90A16569
Distribution Limits
Public
Copyright
Other

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