VOYAGER
Voyager LECP Data Analysis Handbook
In-Flight Calibration Studies
v1ebe.dat
c c "v1ebe.dat" c c voyager 1 ebeta energy channel data include file c electron version, e beta & e gamma channels c ----------------------------------------------- c c data are : c el - lower energy of channel in mev c eu - upper energy of channel in mev c dele - channel width in mev ( dele=eu-el ) c epsg - epsilon*gf, in cm**2-sr c all are dimensioned eight (8) c ----------------------------------------------------- el(1) = 0.026 el(2) = 0.037 el(3) = 0.070 el(4) = 0.130 c omit e beta 5 c el(5) = 0.183 c 3 e-gamma channels (eg6-eg7,eg7-eg8,eg8-eg9) el(5) = 1.5 !esa0 lower limit el(6) = 0. el(7) = 0. el(8) = 0 c eu(1) = 0.037 eu(2) = 0.070 eu(3) = 0.130 eu(4) = 0.200 c eu(5) = 0.50 !omit eb05 eu(5) = 8.5 !esb0 lower limit eu(6) = 0. eu(7) = 0. eu(8) = 0
do i = 1,8 dele(i) = eu(i) - el(i) end do
do i = 1,5 epsg(i) = 6.0e-3 emid(i) = sqrt( el(i)*eu(i) ) emidl(i) = alog10( emid(i) ) end do
epsg(4) = 3.9e-3 epsg(5) = 0.12
do i = 6, 8 epsg(i) = 0. emid(i) = 0. emidl(i) = 0. end do c -----------------------------------------------------
v1plo.dat
c c "v1plo.dat" c c voyager 1 plo energy channel data include file c ----------------------------------------------- c c data are : c el - lower energy of channel in mev c eu - upper energy of channel in mev c dele - channel width in mev ( dele=eu-el ) c epsg - epsilon*gf, in cm**2-sr c all are dimensioned eight (8) c ----------------------------------------------------- el(1) = 0.040 el(2) = 0.053 el(3) = 0.085 el(4) = 0.139 el(5) = 0.220 el(6) = 0.550 el(7) = 1.050 el(8) = 2.000 c eu(1) = 0.053 eu(2) = 0.085 eu(3) = 0.139 eu(4) = 0.220 eu(5) = 0.550 eu(6) = 1.050 eu(7) = 2.000 eu(8) = 4.000 c do 10 i = 1,8 10 dele(i) = eu(i) - el(i) c do 20 i = 1,8 epsg(i) = 0.040 emid(i) = sqrt( el(i)*eu(i) ) 20 emidl(i) = alog10( emid(i) ) c epsg(1) = 0.016 c -----------------------------------------------------
v2ebe.dat
c c "v2ebe.dat" c c voyager 2 ebeta energy channel data include file c electron version, e beta & e gamma channels c ----------------------------------------------- c c data are : c el - lower energy of channel in mev c eu - upper energy of channel in mev c dele - channel width in mev ( dele=eu-el ) c epsg - epsilon*gf, in cm**2-sr c all are dimensioned eight (8) c ----------------------------------------------------- el(1) = 0.022 el(2) = 0.035 el(3) = 0.061 el(4) = 0.112 c omit e beta 5 c el(5) = 0.183 c 3 e-gamma channels (eg6-eg7,eg7-eg8,eg8-eg9) el(5) = 0.252 el(6) = 0.480 el(7) = 0.853 el(8) = 0 c eu(1) = 0.035 eu(2) = 0.061 eu(3) = 0.112 eu(4) = 0.183 c eu(5) = 0.50 eu(5) = 0.480 eu(6) = 0.853 eu(7) = 1.200 eu(8) = 0 c do 10 i = 1,7 10 dele(i) = eu(i) - el(i) c do 20 i = 1,7 epsg(i) = 6.0e-3 emid(i) = sqrt( el(i)*eu(i) ) 20 emidl(i) = alog10( emid(i) ) c emid(8) = 0.0 emidl(8) = 0.0
epsg(4) = 3.9e-3 c epsg(5) = 2.0e-3 epsg(5) = 8.1e-3 epsg(6) = 3.5e-3 epsg(7) = 1.1e-4 c -----------------------------------------------------
v2plo.dat
c c "v2plo.dat" c c voyager 2 plo energy channel data include file c ----------------------------------------------- c c data are : c el - lower energy of channel in mev c eu - upper energy of channel in mev c dele - channel width in mev ( dele=eu-el ) c epsg - epsilon*gf, in cm**2-sr c all are dimensioned eight (8) c ----------------------------------------------------- el(1) = 0.028 el(2) = 0.043 el(3) = 0.080 el(4) = 0.137 el(5) = 0.215 el(6) = 0.540 el(7) = 0.990 el(8) = 2.140 c eu(1) = 0.043 eu(2) = 0.080 eu(3) = 0.137 eu(4) = 0.215 eu(5) = 0.540 eu(6) = 0.990 eu(7) = 2.140 eu(8) = 3.500 c do 10 i = 1,8 10 dele(i) = eu(i) - el(i) c do 20 i = 1,8 epsg(i) = 0.113 emid(i) = sqrt( el(i)*eu(i) ) 20 emidl(i) = alog10( emid(i) ) c c -----------------------------------------------------
This is a revised list of geometric factors and passbands for Voyager 2 electron channels based on the analysis of Saturnian and Jovian encounter data. (9/30/82)
Name | Low | High | Delta E | Geo. Fct. | Geo. Mean Energy |
1/G*Delta E |
EB01 | .0224 | .035 | .013 | 0.006 | .028 | 1.28 E4 |
EB02 | .035 | .061 | .026 | 0.006 | .046 | 6.41 E3 |
EB03 | .061 | .112 | .051 | .006 | .083 | 3.27 E3 |
EB04 | .112 | .183 | .071 | .0039 | .143 | 3.61 E3 |
EB05 | all background | |||||
EG6-7 | .252 | .480 | .228 | .0081 | .348 | 541. |
EG7-8 | .480 | .853 | .373 | .0035 | .640 | 766. |
EG8-9 | .853 | 1.20 | .347 | 1.14 E-4 | 1.01 | 2.53 E4 |
ESA0-B0 | 1.5 | 8.5 | 7.0 | .12 | 3.6 | 1.19 |
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Updated 8/9/19, Cameron Crane
VOYAGER 1 ELAPSED TIME
--:--:--:--
Days: Hours:
Minutes: Seconds
*Since official launch
September 5, 1977, 12:56:00:00 UTC
*Since official launch
September 5, 1977, 12:56:00:00 UTC
VOYAGER 2 ELAPSED TIME
--:--:--:--
Days: Hours:
Minutes: Seconds
*Since official launch
August 20, 1977, 14:29:00:00 UTC
*Since official launch
August 20, 1977, 14:29:00:00 UTC
QUICK FACTS
Manufacturer:
Voyagers 1 and 2 were built in the Jet Propulsion
Laboratory in Southern California.
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.
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.