Voyager In Space

 

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VOYAGER

Voyager LECP Data Analysis Handbook

 

Calibrations and Channel Definitions

 

Passbands and Geometric Factors for Voyager 2 LECP

 

FAT #

Name

Low (MeV/Nuc.)

High (MeV/Nuc.)

Mean (MeV/Nuc.)

Geometrical Factor (cm2 SR)

Logic
1 EB01 0.013 0.035 0.020 0.00600   
2 EBD1 0.013 0.035 0.020 0.00012   
3 EB02 0.035 0.061 0.045 0.00600   
4 EBD2 0.035 0.061 0.045 0.00012   
5 EB03 0.061 0.112 0.090 0.00600   
6 EBD3 0.061 0.112 0.090 0.00012   
7 EB04 0.112 0.183 0.120 0.00600   
8 EBD4 0.112 0.183 0.120 0.00012   
9 EB05 0.183 0.500 0.200 0.00600   
10 EBD5 0.183 0.500 0.200 0.00012   
11 EG06 0.252 2.000 0.250 0.00200   
12 EG07 0.480 2.000 0.500 0.00200   
13 EG08 0.853 2.000 0.900 0.00200   
14 EG09 2.100 5.000 2.000 0.00200   
15 E44 0.350 1.500 0.500 1.31000   
16 E45 2.000 100. 2.000 1.31000   
17 E37 6.000 100. 6.000 1.31000   
18 PL01 0.024 0.048 0.025 0.12000   
19 PL02 0.048 0.080 0.050 0.12000   

20

 PL03 0.080 0.137 0.100 0.12000   

21

 PL04 0.137 0.215 0.150 0.12000   

22

 PL05 0.215 0.540 0.250 0.12000   

23

 PL06 0.540 0.990 0.600 0.12000   

24

 PL07 0.990 2.140 1.000 0.12000   

25

 PL08 2.140 3.500 2.500 0.12000   

26

 P32 0.330 0.610 0.350 0.09750 E0E2(E3)

27

 P1 0.520 1.450 0.600 0.44100 E1E2(E3)

28

 P10 4.400 11.400 5.000 0.53900 E2E3(E4)

29

 P11 11.400 20. 12. 0.53900 E2E3(E4)

30

 P16 3.040 17. 5. 1.50000 E5E4(E3)

31

 P23 22. 30. 25. 1.31000 E5E4E3(E2)

32

 P27 37. 89. 50. 1.20000 E5E4E3E2

33

 P31 213. 1000. 250. 1.31000 E4E3

34

 A39 0.091 0.233 0.100 0.09750 E0(E2)

35

 A33 0.230 0.480 0.350 0.09750 E0E2(E3)

36

 A46 0.147 2.0 0.6 0.44100 "D1F1,CA"

37

 A3 0.420 1.7 0.6 0.44100 E1E2(E3)

38

 A4 1.800 4.0 2.5 0.44100 E1E2(E3L12)

39

 A12 4.200 7.8 5.0 0.53900 E2E3(E4L23)

40

 A13 7.800 20. 15. 0.53900 E2E3(E4L23)

41

 A17 3.000 58. 5. 1.50000 E5E4(E3L54)

42

 A24 22. 30. 25. 1.31000 E5E4E3(E2)

43

 A28 31. 56. 50. 1.20000 E5E4E3E2

44

 AL01 1.040 1.850 1.000 0.12000 CALC.

45

 AL02 1.850 3.700 2.500 0.12000 CALC.

46

 M34 0.230 0.440 0.200 0.09750 E0E2

47

 L5 0.710 5.600 1.500 0.44100 E1E2(E3L12)

48

 L14 5.800 28. 6. 0.53900 E2E3(E4L23)

49

 L18 3.900 20. 5. 1.50000 E5E4(E3L54)

50

 M38 0.060 0.200 0.100 0.09750 E0(E2)

51

 M35 0.200 0.340 0.250 0.09750 E0E2(E3)

52

 M47 0.124 14.300 0.250 0.44100 D1F2

53

 M6 0.470 5.200 0.500 0.44100 E1E2(E3L12)

54

 M7 5.200 8.200 6.000 0.44100 E1E2(E3L12)

55

 M15 8.600 40.000 15.000 0.53900 E2E3(E4L23)

56

 M19 6.000 9.200 6.000 1.50000 E5E4(E3L54)

57

 M20 9.600 42. 15. 1.50000 E5E4(E3L54)

58

 M25 44. 61. 50. 1.31000 E5E4E3(E2)

59

 M29 69. 270. 70. 1.20000 E5E4E3E2

60

 H36 0.099 0.140 0.100 0.09750 E0(E2)

61

 H8 0.280 1.900 0.350 0.44100 E1E2(E3)

62

 H9 2.000 12. 2. 0.44100 E1E2(E3)

63

 H43 11.800 74. 15. 0.53900 E2E3(E4)

64

 H21 8.200 17. 10. 1.50000 E5E4(E3L54)

65

 H22 18. 82. 25. 1.50000 E5E4(E3L54)

66

 H26 86. 120. 100. 1.31000 E5E4E3

67

 H30 127. 1000. 150. 1.20000 E5E4E3E2

68

 AR             SINGLES

69

 E0             SINGLES

70

 E1             SINGLES

71

 E2             SINGLES

72

 E3             SINGLES

73

 E4             SINGLES

74

 E5             SINGLES

75

 AL             SINGLES

76

 ALAR             SINGLES

77

 ESA0 2.500 99.999 2.500 0.49350 A-B COINC.

78

 ESB0 8.500 99.999 8.500 0.94620 B 4 PI SR

79

 AB10 8.500 99.999 8.500 0.05040 A-B COINC.

80

 DP09 0.285 5.020 0.250 0.00084 DELTA'

81

 DP10 0.480 2.580 0.600 0.00084 DELTA'

82

 DP11 0.725 1.640 1.000 0.00084 DELTA'

83

 PD09 0.285 5.250 0.250 0.00260 DELTA

84

 PD10 0.480 2.720 0.600 0.00260 DELTA

85

 PD11 0.725 1.580 1.000 0.00260 DELTA

86

 AB12 54.000 87.300 50.000 0.05040 A-B COINC.

87

 AB13 87.300 152.000 100.000 0.05040 A-B COINC.

88

 PSA1 15.800 158.000 15.000 0.49350 A 2 PI SR

89

 PSA2 15.800 49.000 25.000 0.49350 A 2 PI SR

90

 PSA3 16.300 26.200 25.000 0.49350 A 2 PI SR

91

 PSB1 54.000 174.000 50.000 0.94620 B 4 PI SR

92

 PSB2 54.000 87.300 50.000 0.94620 B 4 PI SR

93

 PSB3 54.000 59.000 50.000 0.94620 B 4 PI SR

94

 DA03 0.480 2.450 0.600 0.00084 DELTA'

95

 DA04 0.780 1.410 1.000 0.00084 DELTA'

96

 DZ01 0.405 18.800 0.600 0.00084 DELTA'

97

 AD033 0.4800.480 2.580 0.600 0.00260 DELTA

98

 AD044 0.7800.780 1.480 1.000 0.00260 DELTA

99

 ZD011 0.4000.400 19.800 0.600 0.00260 DELTA

100

 Sparee                 

 

NOTE: Channels 77-99 here are duplicated from Voyager 1 and should be considered nominal only.

 

Additional material:

 

C PASSBANDS,BACKGROUNDS,AND GEOMETRIC FACTORS FOR PTM,VOYAGER II 
C DECEMBER 27,1977 
C       THRESHOLDS 
FAT  NAME    LOW    HIGH    MEAN    BKGRND     G.F.    TEXT  
 #        (MEV/N) (MEV/N) (MEV/N) (C/SEC.) (CMSQSR)
 1.  EB01 0.0125  0.0350  0.0200 0.0000000 0.002000 1 0 0 0 1  
 2.  EBD1 0.0125  0.0350  0.0200 0.0000000 0.002000 1 4 0 0 1  
    *S ** 1.00 1.00 1.00 1.00 1.00 1.00 1.00 
 3.  EB02 0.0350  0.0610  0.0450 0.0000000 0.002000 1 0 0 0 1  
 4.  EBD2 0.0350  0.0610  0.0450 0.0000000 0.002000 1 4 0 0 1  
    *S ** 1.00 1.00 1.00 1.00 1.00 1.00 1.00 
 5.  EB03 0.0610  0.1120  0.0900 0.0000000 0.002000 1 0 0 0 2  
 6.  EBD3 0.0610  0.1120  0.0900 0.0000000 0.002000 1 4 0 0 2  
    *S ** 1.00 1.00 1.00 1.00 1.00 1.00 1.00 
 7.  EB04 0.1120  0.1830  0.1200 0.0000000 0.002000 1 0 0 0 3  
 8.  EBD4 0.1120  0.1830  0.1200 0.0000000 0.002000 1 4 0 0 3  
    *S ** 1.00 1.00 1.00 1.00 1.00 1.00 1.00 
 9.  EB05 0.1830  0.5000  0.2000 0.0000000 0.002000 1 0 0 0 4  
10.  EBD5 0.1830  0.5000  0.2000 0.0000000 0.002000 1 4 0 0 4  
    *S ** 1.00 1.00 1.00 1.00 1.00 1.00 1.00 
11.  EG06 0.2520  2.0000  0.2500 0.0000000 0.002000 1 0 0 0 5  
12.  EG07 0.4800  2.0000  0.5000 0.0000000 0.002000 1 0 0 0 5  
13.  EG08 0.8530  2.0000  0.9000 0.0000000 0.002000 1 0 0 0 6  
14.  EG09 2.1000  5.0000  2.0000 0.0000000 0.002000 1 0 0 0 7  
15.  E 44 0.3500  1.5000  0.5000 0.0000000 1.310000 1 0 0 035  
16.  E 45 2.0000  100.00  2.0000 0.0000000 1.310000 1 0 0 035  
17.  E 37 6.0000  100.00  6.0000 0.0000000 1.310000 1 0 0 035  
18.  PL01 0.0235  0.0475  0.0250 0.0000000 0.120000 1 0 0 0 8  
19.  PL02 0.0475  0.0795  0.0500 0.0000000 0.120000 1 0 0 0 8  
20.  PL03 0.0795  0.1370  0.1000 0.0000000 0.120000 1 0 0 0 9  
21.  PL04 0.1370  0.2150  0.1500 0.0000000 0.120000 1 1 21111  
    *A ** 0.0343  0.0538 
22.  PL05 0.2150  0.5400  0.2500 0.0000000 0.120000 1 1 21212  
    *A ** 0.0538  0.1350 
23.  PL06 0.5400  0.9900  0.6000 0.0000000 0.120000 1 1 31313  
    *A ** 0.1350  0.2475 
24.  PL07 0.9900  2.1400  1.0000 0.0000000 0.120000 1 1 31414  
    *A ** 0.2475  0.5500 
25.  PL08 2.1400  3.5000  2.5000 0.0000000 0.120000 1 1 41414  
    *A ** 0.5500  1.0000 
26.  P 32 0.3300  0.6100  0.3500 0.0000000 0.097500 1 0 0 035 E0E2(E3)
27.  P  1 0.5200  1.4500  0.6000 0.0000000 0.441000 1 0 0 016 E1E2(E3)
28.  P 10 4.4000  11.400  5.0000 0.0000000 0.539000 1 0 0 016 E2E3(E4)
29.  P 11 11.400  20.000  12.000 0.0000000 0.539000 1 0 0 017 E2E3(E4)
30.  P 16 3.0400  17.300  5.0000 0.0000000 1.500000 1 0 0 018 E5E4(E3)
31.  P 23 22.000  30.000  25.000 0.0000000 1.310000 1 0 0 018 E5E4E3(E2) 
32.  P 27 37.000  89.000  50.000 0.0000000 1.200000 1 0 0 018 E5E4E3E2
33.  P 31 212.60  1000.0  250.00 0.0000000 1.310000 1 0 0 036 E4E3 CA
34.  A 39 0.0910  0.2330  0.1000 0.0000000 0.097500 1 2122620 E0(E2) 
   * M ** 0.0240  0.0530 
35.  A 33 0.2300  0.4800  0.3500 0.0000000 0.097500 1 0 0 021 E0E2(E3)
36.  A 46 0.1470  2.0000  0.6000 0.0000000 0.441000 1 0 0 021 D1F1,CA
37.  A  3 0.4200  1.7000  0.6000 0.0000000 0.441000 1 0 0 022 E1E2(E3)
38.  A  4 1.8000  4.0000  2.5000 0.0000000 0.441000 1 0 0 023 E1E2(E3L12 
39.  A 12 4.2000  7.8000  5.0000 0.0000000 0.539000 1 0 0 024 E2E3(E4L23 
40.  A 13 7.8000  20.000  15.000 0.0000000 0.539000 1 0 0 024 E2E3(E4L23 
41.  A 17 3.0000  58.000  5.0000 0.0000000 1.500000 1 2183025 E5E4(E3L54 
    *M ** 176.00  1000.0                                     CONTAMINANT 
42.  A 24 22.000  30.000  25.000 0.0000000 1.310000 1 0 0 025 E5E4E3(E2  
43.  A 28 31.000  56.000  50.000 0.0000000 1.200000 1 2183025 E5E4E3E2
    *M ** 270.00  1000.0                                      CONTAMINAN 
44.  AL01 1.0400  1.8500  1.0000 0.0000000 0.120000 1 2142819 CALC.  
    *M ** 0.2700  0.4800                                      CONTAMINAN 
45.  AL02 1.8500  3.7000  2.5000 0.0000000 0.120000 1 2142819 CALC.  
    *M ** 0.5100  1000.0                                      CONTAMINAN 
46.  A 34 0.2300  0.4400  0.2000 0.000000  0.097500 1 0 0 021 E0 E2 CALC 
47.  L  5 0.7100  5.6000  1.5000 0.000000  0.441000 1 0 0 036 E1E2(E3L12 
48.  L 14 5.8000  28.000  6.0000 0.000000  0.539000 1 0 0 036 E2E3(E4L23 
49.  L 18 3.9000  20.000  5.0000 0.000000  1.500000 1 0 0 036 E5E4(E3L54 
50.  M 38 0.0600  0.2000  0.1000 0.000000  0.097500 1 3203126 E0(E2) 
    *H ** 0.0150  0.0900                                      CONTAMINAN 
51.  M 35 0.2000  0.3400  0.2500 0.000000  0.097500 1 3203126 E0 E2(E3)  
    *N ** 0.1600  0.2800                                      CONTAMINAN 
52.  M 47 0.1240  14.300  0.2500 0.000000  0.441000 1 3203127 D1F2 CALC  
    *H ** 0.0310  768.00                                      CONTAMINAN 
53.  M  6 0.4700  5.2000  0.5000 0.000000  0.441000 1 3213228 E1E2(E3L12 
    *N ** 0.4300  4.0000                                      CONTAMINAN 
54.  M  7 5.2000  8.2000  6.0000 0.000000  0.441000 1 0 0 028 E1E2(E3L12 
55.  M 15 8.6000  40.000  15.000 0.000000  0.539000 1 3233329 E2E3(E4L23 
    *N ** 9.9000  44.000                                      CONTAMINAN 
56.  M 19 6.0000  9.2000  6.0000 0.000000  1.500000 1 3243430 E5E4(E3L54 
    *N ** 6.6000  8.6000                                      CONTAMINAN 
57.  M 20 9.6000  42.000  15.000 0.000000  1.500000 1 3243430 E5E4(E3L54 
    *N ** 9.2000  36.000                                      CONTAMINAN 
58.  M 25 44.000  61.000  50.000 0.000000  1.310000 1 3243430 E5E4E3(E2) 
    *N ** 61.700  74.000                                      CONTAMINAN 
59.  M 29 69.000  270.00  70.000 0.000000  1.200000 1 3243430 E5E4E3 E2  
    *N ** 101.00  1000.0                                      CONTAMINAN 
60.  H 36 0.0990  0.1400  0.1000 0.000000  0.097500 1 0 0 031 E0(E2) CAL 
61.  H  8 0.2800  1.9000  0.3500 0.000000  0.441000 1 0 0 032 E1E2(E3 CA 
62.  H  9 2.0000  12.000  2.0000 0.000000  0.441000 1 0 0 032 E1E2(E3 CA 
63.  H 43 11.800  74.000  15.000 0.000000  0.539000 1 0 0 033 E2E3(E4 CA 
64.  H 21 8.2000  17.000  10.000 0.000000  1.500000 1 0 0 034 E5E4(E3L54 
65.  H 22 18.000  82.000  25.000 0.000000  1.500000 1 0 0 034 E5E4(E3L54 
66.  H 26 86.000  120.00  100.00 0.000000  1.310000 1 0 0 034 E5E4E3 CAL 
67.  H 30 127.00  1000.0  150.00 0.000000  1.200000 1 0 0 034 E5E4E3E2 C 
68.  S E0  
69.  S E1  
70.  S E2  
71.  S E3  
72.  S E4  
73.  S E5  
74.  S AL  
75.  S AR  
76.  ALAR  
77.  SPARE 
78.  SPARE 
79.  SPARE 
80.  SPARE 
81.  SPARE 
82.  SPARE 
83.  SPARE 
84.  SPARE 
85.  SPARE 
86.  SPARE 
87.  SPARE 
88.  SPARE 
89.  SPARE 
90.  SPARE 
91.  SPARE 
92.  SPARE 
93.  SPARE 
94.  SPARE 
95.  SPARE 
96.  SPARE 
97.  SPARE 
98.  SPARE 
99.  SPARE 
00.  SPARE 
*** THIS IS A FILE DESCRIBING THE FORMULAS FOR CALCULATION OF SPECTRAL
     EXPONENTS.
   
     GAMMA=C1*(LOG10(RATIO)+C2)  
   
ITEM. NAME FAT FILE IDS. COEFFS.OF FIT 1    BOUNDARY  COEFFS. OF FIT 2
 #         NUM.  DENOM.    C1      C2         RATIO     C1      C2
 1   EB12     1     3   -2.486  0.1920  3.4000   -3.076  0.0550  
 2   EB23     3     5   -3.993  0.2930 
 3   EB34     5     7   -3.998  0.1680  2.0000   -4.134  0.1400  
 4   EB45     7     9   -3.822  0.1920  1.0200   -2.913  0.6650  
 5   EG67    11    12   -3.839  0.1890  1.7500   -10.15 -0.0830  
 6   EG78    12    13   -4.728  0.0580  2.0000   -10.33 -0.1380  
 7   EG89    13    14   -2.541  0.4050 
 8   PL12    18    19   -3.688 +0.1160 
 9   PL23    19    20   -4.372  0.2520 
10   PL34    20    21   -4.611  0.1310 
11   PL45    21    22   -4.106  0.5020 
12   PL56    22    23   -2.650  0.2530   3.300   -3.113  0.1330  
13   PL67    23    24   -3.448  0.4090 
14   PL78    24    25   -3.302  0.1301  2.7000   -3.775  0.0636  
15   32/1    26    27   -5.768  0.0843 
16   1/10    27    28   -1.090  0.8730 
17   1011    28    29   -2.760  0.1550 
18   1623    30    31   -1.970 -0.2510  13.000   -1.390  0.0114  
19   AL12    44    45   -3.692  0.3712 
20   3933    34    35   -2.754  0.2774  5.0000   -1.133  1.6060  
21   33/3    35    37   -2.190  0.7200  0.7000   -3.200  0.5230  
22    3/4    37    38   -2.090  0.2353  10.000   -1.704  0.4260  
23   4/12    38    39   -3.100  0.2139 
24   1213    39    40   -2.800  0.5300 
25   1724    41    42   -2.250 -0.5550  40.000   -1.300  0.1930  
26   3835    50    51   -2.640 -0.0414  10.000   -1.390  0.8120  
27   35/6    51    53   -1.080  1.4900  0.8200   -1.990  0.8730  
28    6/7    53    54   -1.220  0.1670  9.9000   -1.120  0.3500  
29   7/15    54    55   -1.850  1.2100  0.5500   -2.290  1.0400  
30   1920    56    57   -2.260  1.1100  0.8600   -4.090  0.6270  
31   36/8    60    61   -1.090  2.7000  0.0680   -1.490  2.2300  
32    8/9    61    62   -1.730  0.3700  1.6000   -1.210  0.5980  
33   9/43    62    63   -1.650  0.8150 
34   2122    64    65   -2.720  0.3190 
35 
36 
37 
38 
39 
40 
41 
42 
43 
44 
45 
46 
47 
48 
49 
50 
***THIS FILE IS FOR INITIALIZATION OF THE ABUNDANCE RATIO CALCULATIONS
  THE FORM OF THE EMPIRICAL EXPRESSION USED IN THE CALCULATIONS IS:  
*  
*  LOG(P/ALPHA)=LOG(C.R.RATIO)/(A*GAMMA**2+B*GAMMA + C)  
*  
ITEM  NUMERS. DENOMS.IG. NAME      A       B       C    GFL GFU  DEF.
  1  20 00 00  34 00 10 PL3/39  -0.0016 -0.1752 -0.3896 -1.5 1.0 -1.5
  2  21 22 00  35 00 11 P45/33  +0.0305 -0.0517  0.2091 -1.5 1.0 -1.5
  3  23 24 00  37 00 13 P6+7/3   0.0073  0.0929  0.0999 -1.5 1.0 -1.5
  4  27 00 00  37 00 16  P1/A3  -0.0242 -0.1517 -0.5862 -6.0 1.0 -3.0
  5  28 00 00  39 00 17  10/12   0.0082  0.1097  0.2903 -6.0 1.0 -3.0
  6  29 00 00  40 00 17  11/13  -0.0091  0.0635 -0.1534 -6.0 1.0 -3.0
  7  24 00 00  44 00 14 PL7/A1   0.0132  0.0200  0.1549 -1.5 1.0 -3.0
  8  25 00 00  38 00 14 PL8/ 4   0.0078 -0.0236 -0.2024 -1.5 1.0 -3.0
  9  30 00 00  41 00 18  16/17  -0.0199 -0.1595 -0.3234 -6.0-1.0 -3.0
 10  31 00 00  42 00 18  23/24  -0.0000  0.0000  1.0000 -6.0 1.0 -3.0
 11  32 00 00  43 00 18  27/28   0.0066  0.1587  0.3598 -6.0-1.5 -3.0
 12  34 00 00  50 00 20  39/38   0.0007  0.1181 -0.0990 -3.0 1.0 -3.0
 13  35 00 00  51 00 21  33/35   0.0012  0.1468  0.1944 -6.0 1.0 -3.0
 14  37 38 00  53 00 22  3+4/6   0.0007 -0.0444 -0.0851 -6.0 1.0 -3.0
 15  39 00 00  54 00 24   12/7  -0.0087 -0.0163  0.2313 -6.0 1.0 -3.0
 16  40 00 00  55 00 24  13/15  -0.0210 -0.2255 -0.4396 -6.0 1.0 -3.0
 17  41 00 00  56 00 25  17/19   0.0754  0.3432  1.1263 -6.0-1.5 -3.0
 18  42 43 00  57 58 25 248205  -0.0179  0.2029 -0.1130 -6.0-1.0 -3.0
 19  36 00 00  52 00 22 D1F1/2  -0.0933 -0.6182 -0.8421 -3.0 1.0 -3.0
 20  50 00 00  60 00 26  38/36   0.0541 -0.0913  0.5999 -6.0 1.0 -3.0
 21  53 00 00  61 00 28    6/8   0.0112  0.1544 -0.3327 -6.0 1.0 -3.0
 22  54 00 00  62 00 29    7/9  -0.0132 -0.0238 -1.0944 -6.0 1.0 -3.0
 23  55 00 00  63 00 29  15/43  -0.0010 -0.1391 -0.7203 -6.0 1.0 -3.0
 24  56 57 58  64 65 30 192521  -0.0042 -0.1952 -0.3288 -6.0 1.0 -3.0
 25  
 26  
 27  
 28  
 29  
 30  
***THIS FILE IS FOR THE CALCULATION OF ANGULAR DISTRIBUTION RATIOS
*  INCLUDING CORRECTIONS FOR SPECTRUM AND RELATIVE GEOMETRIC FACTORS 
*   RATIO=(C.R.RATIO)/(A*GAMMA**2+B*GAMMA+C) 
ITEM  NUMS. DENOMS.  
 1  028 029  030 000 10+11/16  -0.0086 +0.0922 +0.0345 -6.0 +1.0 
 2  039 040  041 000 12+13/17  -0.0235 -0.0510 -1.3979 -6.0 -1.0 
 3  055 000  056 057 15/19+20  -0.0163  0.0289 -0.0785 -6.0 +1.0 
 4  063 000  064 065 43/21+22  -0.0145 -0.0423  0.1165 -6.0  1.0 
*  
*  
* THIS FILE IS FOR THE CALCULATION OF POLAR/EQUATORIAL RATIOS FOR
* E-BETA'/E-BETA.  NO CORRECTION FOR PASSBAND WILL BE MADE AT THIS
* TIME.  WE WILL USED EMPIRICALLY DERIVED RELATIVE GEOMETRIC FACTORS 
* AS SOON AS THEY ARE AVAILABLE FROM FLIGHT DATA.  WE WILL USE A SIMILAR 
* FORM T TO THE OTHER CALULCATIONS.  
*  
*  (POLAR/EQUATOR)=(C.R.POLAR/C.R.EQUAT.)*(G.F.EQUATOR/G.F.POLAR)
   
ITEM NUM. DEN. NAME      SEC 1 SEC 2 SEC 3 SEC 4 SEC 5 SEC 6 SEC 7
  5  001  002  EBD1/EB01  1.00  1.00  1.00  1.00  1.00  1.00  1.00
  6  003  004  EBD2/EB02  1.00  1.00  1.00  1.00  1.00  1.00  1.00
  7  005  006  EBD3/EB03  1.00  1.00  1.00  1.00  1.00  1.00  1.00
  8  007  008  EBD4/EB04  1.00  1.00  1.00  1.00  1.00  1.00  1.00
  9  009  010  EBD5/EB05  1.00  1.00  1.00  1.00  1.00  1.00  1.00
 10  
 11  
 12  
 13  
 14  
 15  
 16  
 17  
 18  
 19  
 20

 

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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

VOYAGER 2 ELAPSED TIME

--:--:--:--
Days: Hours: Minutes: Seconds

*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.