Voyager LECP Data Analysis Handbook
In-Flight Calibration Studies
Study of Voyager 2 LECP Responses in Partial Exposure ("Chicken") Mode
Thomas P. Armstrong
and
Dong Feng Lu
TABLE 1
List of "before/after" Count Rate Ratios for Inbound Entry and Outbound Exit from Chicken Mode
INBOUND ENTRY | OUTBOUND EXIT | |||||||
---|---|---|---|---|---|---|---|---|
CHANNEL |
Sector 7 | Sector 8 | Sector C | RATIO | Sector 7 | Sector 8 | Sector C | RATIO |
PL01 | 8563.361 | 444.529 | 1042.241 | 13.583 | 5457.778 | 272.430 | 445.114 | 30.028 |
PL02 | 10131.093 | 345.964 | 1140.948 | 12.309 | 8096.444 | 273.795 | 563.705 | 26.983 |
PL03 | 6756.303 | 154.720 | 674.892 | 12.691 | 6617.333 | 150.804 | 419.935 | 24.027 |
PL04 | 3885.333 | 74.707 | 347.484 | 13.970 | 4631.112 | 80.879 | 255.235 | 26.097 |
PL05 | 3170.370 | 23.652 | 242.632 | 14.370 | 5255.111 | 26.794 | 243.606 | 24.115 |
PL06 | 496.296 | 0.539 | 30.132 | 16.753 | 1383.111 | 1.981 | 69.741 | 20.383 |
PL07 | 133.333 | 0.196 | 7.336 | 18.648 | 378.000 | 0.498 | 21.901 | 17.638 |
PL08 | 20.000 | 0.101 | 0.946 | 23.553 | 56.194 | 0.105 | 2.436 | 24.057 |
0001 | 644.334 | 3.080 | 17.247 | 45.264 | 1952.889 | 4.815 | 34.860 | 64.838 |
0003 | 14.646 | 2.883 | 2.978 | 123.078 | 81.875 | 3.445 | 3.606 | 486.898 |
0032 | 27.854 | 0.000 | 0.464 | 60.034 | 59.778 | 0.000 | 0.768 | 77.869 |
0033 | 22.167 | 0.000 | 0.321 | 68.963 | 53.729 | 0.000 | 0.543 | 98.946 |
0035 | 4.125 | 0.000 | 0.110 | 37.643 | 9.736 | 0.000 | 0.127 | 76.368 |
0038 | 90.667 | 0.000 | 1.590 | 57.021 | 148.222 | 0.000 | 2.655 | 55.827 |
0039 | 332.193 | 0.011 | 12.664 | 26.254 | 341.028 | 0.014 | 5.897 | 57.965 |
Note: Ratio is computed as (Sector 7 - Sector 8)/(Sector C - Sector 8) where Sector 8 is shield-penetrating background, Sector 7 is the full intensity for an "open" sector and Sector C is the "Chicken" sector in which the LECP was moved through two 1.8 degree steps from the background or shielded position towards the open, or normal position. 45 degrees of rotation, or 25 1.8 degree steps are required for full sector movement.
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Updated 8/9/19, Cameron Crane
VOYAGER 1 ELAPSED TIME
*Since official launch
September 5, 1977, 12:56:00:00 UTC
VOYAGER 2 ELAPSED TIME
*Since official launch
August 20, 1977, 14:29:00:00 UTC
QUICK FACTS
Mission Duration: 40+ years have elapsed for both Voyager 1 and Voyager 2 (both are ongoing).
Destination: Their original destinations were Saturn and Jupiter. Their current destination is interstellar space.