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Lunar and Planetary Missions Launched from a Geosynchronous Transfer Orbit

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dc.contributor.author Penzo, P. en_US
dc.date.accessioned 2004-09-25T23:49:36Z
dc.date.available 2004-09-25T23:49:36Z
dc.date.issued 1997-02-10 en_US
dc.identifier.citation Huntsville, AL, USA en_US
dc.identifier.clearanceno 97-0148 en_US
dc.identifier.uri http://hdl.handle.net/2014/21757
dc.description.abstract Lithium Lorentz Force Accelerators (LFA's) are capable of processing very high power levels and are therefore applicable to a wide range of challenging missions. For this class of missions, the emphasis must be on achieving high efficiency at an Isp of 4000-5000s at power levels of 200-250 kWe. The engines must demonstrate very reliable operation for a service life of about 3000 hours. en_US
dc.format.extent 585066 bytes
dc.format.mimetype application/pdf
dc.language.iso en_US
dc.subject.other Lithium Lorentz Force Accelerators LFA's Isp power levels engines engine technologies en_US
dc.title Lunar and Planetary Missions Launched from a Geosynchronous Transfer Orbit en_US


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