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Ulysses HISCALE Data Analysis Handbook

 

Appendix 14. LAN EDR Record Map


WORD FMT FRAME FWORD S/C FWD CHAN SECTOR SPIN
841 1 10 1 97 D1 2 4
842 1 10 2 98 C2 2 4
843 1 10 3 99 D2 2 4
844 1 10 4 100 P 2 4
845 1 10 5 101 P1' 3 4
846 1 10 6 102 P2' 3 4
847 1 10 7 103 P3' 3 4
848 1 10 8 104 P4' 3 4
849 1 10 9 105 P5' 3 4
850 1 10 10 106 E1' 3 4
851 1 10 11 107 E2' 3 4
852 1 10 12 108 E3' 3 4
853 1 10 13 109 E4' 3 4
854 1 10 14 110 P6' 3 4
855 1 10 15 111 P7' 3 4
856 1 10 16 112 P8' 3 4
857 1 10 17 113 E5' 3 4
858 1 10 18 114 FP6' 3 4
859 1 10 19 115 FP7' 3 4
860 1 11 0 96 Z2 3 4
861 1 11 1 97 Z2A 3 4
862 1 11 2 98 Z3 3 4
863 1 11 3 99 Z4 3 4
864 1 11 4 100 W1 3 4
865 1 11 5 101 W2 3 4
866 1 11 6 102 W3 3 4
867 1 11 7 103 W4 3 4
868 1 11 8 104 W5 3 4
869 1 11 9 105 W6 3 4
870 1 11 10 106 W7 3 4
871 1 11 11 107 W8 3 4
872 1 11 12 108 C1 3 4
873 1 11 13 109 D1 3 4
874 1 11 14 110 C2 3 4
875 1 11 15 111 D2 3 4
876 1 11 16 112 P 3 4
877 1 11 17 113 P1' 4 4
878 1 11 18 114 P2' 4 4
879 1 11 19 115 P3' 4 4
880 1 12 0 96 P4' 4 4
881 1 12 1 97 P5' 4 4
882 1 12 2 98 E1' 4 4
883 1 12 3 99 E2' 4 4
884 1 12 4 100 E3' 4 4
885 1 12 5 101 E4' 4 4
886 1 12 6 102 P6' 4 4
887 1 12 7 103 P7' 4 4
888 1 12 8 104 P8' 4 4
889 1 12 9 105 E5' 4 4
890 1 12 10 106 FP6' 4 4
891 1 12 11 107 FP7' 4 4
892 1 12 12 108 Z2 4 4
893 1 12 13 109 Z2A 4 4
894 1 12 14 110 Z3 4 4
895 1 12 15 111 Z4 4 4
896 1 12 16 112 W1 4 4
897 1 12 17 113 W2 4 4
898 1 12 18 114 W3 4 4
899 1 12 19 115 W4 4 4
900 1 13 0 96 W5 4 4
901 1 13 1 97 W6 4 4
902 1 13 2 98 W7 4 4
903 1 13 3 99 W8 4 4
904 1 13 4 100 P1 4 4
905 1 13 5 101 P2 4 4
906 1 13 6 102 P3 4 4
907 1 13 7 103 P4 4 4
908 1 13 8 104 E1 4 4
909 1 13 9 105 E2 4 4
910 1 13 10 106 E3 4 4
911 1 13 11 107 E4 4 4
912 1 13 12 108 P5 4 4
913 1 13 13 109 P6 4 4
914 1 13 14 110 P7 4 4
915 1 13 15 111 P8 4 4
916 1 13 16 112 E5 4 4
917 1 13 17 113 FP6 4 4
918 1 13 18 114 FP7 4 4
919 1 13 19 115 DE1 4 4
920 1 14 0 96 DE2 4 4

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Updated 8/8/19, Cameron Crane

QUICK FACTS

Manufacturer: ESA provided the Ulysses spacecraft, NASA provided the power supply, and various others provided its instruments.

Mission End Date: June 30, 2009

Destination: The inner heliosphere of the sun away from the ecliptic plane

Orbit:  Elliptical orbit transversing the polar regions of the sun outside of the ecliptic plane