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Mission Analysis for Laser Interferometer Space Antenna (LISA)

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dc.contributor.author Hechler, F. en_US
dc.contributor.author Folkner, W. M. en_US
dc.date.accessioned 2004-09-30T23:10:11Z
dc.date.available 2004-09-30T23:10:11Z
dc.date.issued 1992 en_US
dc.identifier.clearanceno 96-1256 en_US
dc.identifier.uri http://hdl.handle.net/2014/26393
dc.description.abstract The interplanetary orbits of three pairs of spaceprobes carrying laser interferometer antennae are designed such that their miutual distances, i.e., the lengths of the interferometer arms remain nearly constant. The pairs move relative to each other in an equilateral triangle. en_US
dc.format.extent 374892 bytes
dc.format.mimetype application/pdf
dc.language.iso en_US
dc.subject.other LISA interferometry interferometer en_US
dc.title Mission Analysis for Laser Interferometer Space Antenna (LISA) en_US


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