urn:nasa:pds:lro_minirf_globalmosaic:data_globalmosaic:global_s4_32ppd_simp_0c 1.0 1.19.0.0 Product_Observational 2024-07-19 1.0 Initial PDS4 Version 2009-07-19T12:27:42.785399Z 2010-12-26T09:17:27.6068Z Lunar Reconnaissance Orbiter Mission urn:nasa:pds:context:investigation:mission.lunar_reconnaissance_orbiter data_to_investigation Lunar Reconnaissance Orbiter Host Lunar Reconnaissance Orbiter Spacecraft urn:nasa:pds:context:instrument_host:spacecraft.lro is_instrument_host Mini-RF LRO Instrument Mini-RF is a hybrid dual-polarimetric side-looking synthetic aperture radar (SAR) instrument. urn:nasa:pds:context:instrument:lro.mrflro is_instrument Moon Satellite DDR Johns Hopkins University Applied Physics Laboratory global_s4_32ppd_simp_0c display_settings_to_array Sample Left to Right Line Top to Bottom global_s4_32ppd_simp_0c cartography_parameters_to_image_object -180.0 180.0 90.0 -90.0 Equirectangular 0.0 0.0 0.0 Coordinate Pair 947.6047007546699 947.6047007546699 32.0 32.0 -5458203.076346898 2729101.538173449 Planetocentric MOON 1737.4 1737.4 1737.4 Positive East urn:nasa:pds:lro_minirf_globalmosaic:document:userguide::1.0 data_to_document User guide providing an overview of the Mini-RF Global Mosaic datasets, the file naming convention, data products, and parameter descriptions. urn:nasa:pds:lro_minirf_globalmosaic:document:parameters_summary::1.0 data_to_document This document provides a summary of the Stokes parameters and their relationship to a given Mini-RF Global Mosaic data product. The parameter is determined by the file naming convention as described in the user guide. global_s4_32ppd_simp_0c.img Binary file containing Global Mosaic fourth Stokes Parameter (S4) data at 32.0 pixels per degree resolution. global_s4_32ppd_simp_0c 0 2 Last Index Fastest Global Mosaic image containing The fourth Stokes Parameter (S4); represents the sine of the average phase between the horizontally and vertically polarized components of the received field. S4 = -2Im{H x V_con} where H x V_con is the cross product of the horizontal component of the polarized portion of the received EM field and the complex conjugate of the vertical component of the polarized portion of the received EM field and Im indicates that only the imaginary component of the cross product is used. IEEE754LSBSingle Line 5760 1 Sample 11520 2 -1.7976931E+308 global_s4_32ppd_simp_0c.lbl 0 PDS3 PDS3 label Carriage-Return Line-Feed