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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
281 0 14 1 97 P4' 1 2
282 0 14 2 98 P5' 1 2
283 0 14 3 99 E1' 1 2
284 0 14 4 100 E2' 1 2
285 0 14 5 101 E3' 1 2
286 0 14 6 102 E4' 1 2
287 0 14 7 103 P6' 1 2
288 0 14 8 104 P7' 1 2
289 0 14 9 105 P8' 1 2
290 0 14 10 106 E5' 1 2
291 0 14 11 107 FP6' 1 2
292 0 14 12 108 FP7' 1 2
293 0 14 13 109 Z2 1 2
294 0 14 14 110 Z2A 1 2
295 0 14 15 111 Z3 1 2
296 0 14 16 112 Z4 1 2
297 0 14 17 113 W1 1 2
298 0 14 18 114 W2 1 2
299 0 14 19 115 W3 1 2
300 0 15 0 96 W4 1 2
301 0 15 1 97 W5 1 2
302 0 15 2 98 W6 1 2
303 0 15 3 99 W7 1 2
304 0 15 4 100 W8 1 2
305 0 15 5 101 C1 1 2
306 0 15 6 102 D1 1 2
307 0 15 7 103 C2 1 2
308 0 15 8 104 D2 1 2
309 0 15 9 105 P 1 2
310 0 15 10 106 P1' 2 2
311 0 15 11 107 P2' 2 2
312 0 15 12 108 P3' 2 2
313 0 15 13 109 P4' 2 2
314 0 15 14 110 P5' 2 2
315 0 15 15 111 E1' 2 2
316 0 15 16 112 E2' 2 2
317 0 15 17 113 E3' 2 2
318 0 15 18 114 E4' 2 2
319 0 15 19 115 P6' 2 2
320 0 16 0 96 P7' 2 2
321 0 16 1 97 P8' 2 2
322 0 16 2 98 E5' 2 2
323 0 16 3 99 FP6' 2 2
324 0 16 4 100 FP7' 2 2
325 0 16 5 101 Z2 2 2
326 0 16 6 102 Z2A 2 2
327 0 16 7 103 Z3 2 2
328 0 16 8 104 Z4 2 2
329 0 16 9 105 W1 2 2
330 0 16 10 106 W2 2 2
331 0 16 11 107 W3 2 2
332 0 16 12 108 W4 2 2
333 0 16 13 109 W5 2 2
334 0 16 14 110 W6 2 2
335 0 16 15 111 W7 2 2
336 0 16 16 112 W8 2 2
337 0 16 17 113 P1 2 2
338 0 16 18 114 P2 2 2
339 0 16 19 115 P3 2 2
340 0 17 0 96 P4 2 2
341 0 17 1 97 E1 2 2
342 0 17 2 98 E2 2 2
343 0 17 3 99 E3 2 2
344 0 17 4 100 E4 2 2
345 0 17 5 101 P5 2 2
346 0 17 6 102 P6 2 2
347 0 17 7 103 P7 2 2
348 0 17 8 104 P8 2 2
349 0 17 9 105 E5 2 2
350 0 17 10 106 FP6 2 2
351 0 17 11 107 FP7 2 2
352 0 17 12 108 DE1 2 2
353 0 17 13 109 DE2 2 2
354 0 17 14 110 DE3 2 2
355 0 17 15 111 DE4 2 2
356 0 17 16 112 C1 2 2
357 0 17 17 113 D1 2 2
358 0 17 18 114 C2 2 2
359 0 17 19 115 D2 2 2
360 0 18 0 96 P 2 2

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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