Voyager In Space

 

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VOYAGER
 

Voyager LECP Data Analysis Handbook

 

Calibrations and Channel Definitions

 

Feb. 6, 1979
β Channel                       β
100 KeV into b, Read out on b-1 disc

 

Input Rate Output Rate In Out

(Cycles per Second)

649

649

1.43K

1.43K

12.6K

12.4K

3.02K

3.00K

35.8K

34.0K

8.52K

8.40K

78.9K

68.6K

12.5K

12.2K

132K

102K

18.9K

18.3K

166K

121K

35.4K

33.4K

229K

149K

67.0K

59.2K

316K

176K

134K

103K

501K

203K

156K

113K

633K

214K

242K

151K

324K

174K

431K

190K

630K

206K

 

 

Channel A
Feb. 6, 1979

 

 

A1 One-Shot Out (J11-23)

A2 (FF Out)

A0 (¸ 8 Output FF)

Input
Rate

Output Rate

In

Out

In

Out

(kilo cycles per second)

12.6

12.5

13.7

6.8

12.6

1.61

55.1

49.7

21.8

10.6

20.9

2.69

79

68

41.5

19.7

41.0

5.42

134

102

64.4

29.7

76.9

9.93

196

146

126

54

114

14.7

256

180

175

72

177

23.5

410

254

205

83

353

51.0

676

346

326

116

499

78.8

   

456

142

678

123

   

677

178

   

 

 

 

Feb. 22, 1979

 

D1-D2

 

r = R/(1 + RT) Lifetime = 1 – rT

 

1 + RT = R/r r = R(1 – rT)

 

RT = R/r – 1 r = R – rRT

 

T = 1/r – 1/R = (R – r)/(Rr) r(1 + RT) = R

 

r = R/(1 + RT)

 

r = 100K

 

R = 260K

 

T = (260K – 100K)/((260K)(100K)) = 160K/((260)(100)KK) = 1.6/(260K) = 6.15 μs

 

R 1 + RT r(calc) r(act)
10K 1.062 9.42K 9.6K
20K 1.123 17.8K 18.5K
40K 1.246 32.1K 35K
80K 1.492 53.6K 58K
150K 1.922 78.1K 82K
250K 2.54 98.4K 99K
500K 4.08 123K 110K

 

 

α

 

r = 150K

 

R = 233K

 

T = (233-150)/((233)(150)) = 2.37 μs

 

R

1 + RT

r(calc)

r(act)

20K

1.0474

19.1K

19.1K

40K

1.095

36.5K

37K

80K

1.190

67.2K

68K

150K

1.36

110K

110K

250K

1.59

157K

155K

500K

2.185

229K

201K

600K

2.422

248K

210K


Feb. 22, 1979

 

10 mc Sr90 source from GSFC, thru G-10 cover (1/64")

 

A0 Read out 201 K max; could not see roll-over

 

A1 Read out 190 K max, could not see roll-over

  

 

Return to Calibrations main page.

Return to Voyager LECP Data Analysis Handbook Table of Contents.
Return to Fundamental Technologies Home Page.


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.