Actions for Beam-powered lunar rover design [electronic resource].

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Beam-powered lunar rover design [electronic resource].

Published
Washington, D.C. : United States. National Aeronautics and Space Administration, 1992.
Oak Ridge, Tenn. : Distributed by the Office of Scientific and Technical Information, U.S. Dept. of Energy.
Physical Description
Pages: (45 pages) : digital, PDF file
Additional Creators
Pacific Northwest Laboratory, United States. National Aeronautics and Space Administration, and United States. Department of Energy. Office of Scientific and Technical Information
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Summary
Manned exploration of our nearest neighbors in the solar systems is the primary goal of the Space Exploration Initiative (SEI). An integral part of any manned lunar or planetary outpost will be a system for manned excursions over the surface of the planet. This report presents a preliminary design for a lunar rover capable of supporting four astronauts on long-duration excursions across the lunar landscape. The distinguishing feature of this rover design is that power is provided to rover via a laser beam from an independent orbiting power satellite. This system design provides very high power availability with minimal mass on the rover vehicle. With this abundance of power, and with a relatively small power-system mass contained in the rover, the vehicle can perform an impressive suite of mission-related activity. The rover might be used as the first outpost for the lunar surface (i.e., a mobile base). A mobile base has the advantage of providing extensive mission activities without the expense of establishing a fixed base. This concept has been referred to as Rove First.'' A manned over, powered through a laser beam, has been designed for travel on the lunar surface for round-trip distances in the range of 1000 km, although the actual distance traveled is not crucial since the propulsion system does not rely on energy storage. The life support system can support a 4-person crew for up to 30 days, and ample power is available for mission-related activities. The 8000-kg rover has 30 kW of continuous power available via a laser transmitter located at the Earth-moon L1 libration point, about 50,000 km above the surface of the moon. This rover, which is designed to operate in either day or night conditions, has the flexibility to perform a variety of power-intensive missions. 24 refs.
Report Numbers
E 1.99:pnl-8053
pnl-8053
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Other Subject(s)
Note
Published through SciTech Connect.
03/01/1992.
"pnl-8053"
"DE92011511"
Bamberger, J.A.; Antoniak, Z.I.; Coomes, E.P.; Wise, J.A.; Bates, J.M.; Dagle, J.E.; Dodge, R.E.; Chiu, M.A.
Funding Information
AC06-76RL01830
View MARC record | catkey: 14114765