Voyager In Space

 

Galaxy Banner Image
VOYAGER

Voyager LECP Data Analysis Handbook

 

Data File Descriptions

 

Experiment Data Record (EDR) Format Specification

 

APPENDIX B: Engineering Experiment Data Record Formation

 

The Engineering Record will be used in the engineering EDR and all normal-rate Science EDR's. The Engineering Record Format is described in Figure B-2, the Standard Record Header in Appendix C , and the Engineering Data Block in Figure B-4 and Table B-1. This Engineering data block contains engineering data for 60 EMF for both 10 and 40 bps data. Each channel will appear in the same location during a readout sequence. For 40 and 10 bps data, a readout sequence is accomplished in 12 and 48 minutes respectively. Decommutation must be done with the last Decom Map preceeding the Engineering record.

 

Figure B-2. Engineering Record (965 32-bit words)

 

Standard
Header
(60)
Subhdr
Spares
(5)
Engr
MF 1
(15)
Engr
MF 2
(15)
Eng
MF 3
(15)
Eng
MF 4
(15)
Eng
MF 5
(15). .
Eng
MF 59
. . (15)

Eng
MF 60
(15)

 

 

Figure B-4. Engineering Record Data Block Format

 

EDR
Data Word
Bits
31   24

16

8

0


31   24

16

8

0

1 COM
Position
100
COM
Position
101
COM
Position
102
COM
Position
103
COM
Position
104
COM
Position
105
COM
Position
106
COM
Position
107
3 COM
Position
108
COM
Position
109
COM
Position
110
COM
Position
111
COM
Position
112
COM
Position
113
COM
Position
114
COM
Position
115

:

. . .

13 COM
Position
148
COM
Position
149
COM
Position
150
COM
Position
151
COM
Position
152
COM
Position
153
COM
Position
154
COM
Position
155
15 COM
Position
156
COM
Position
157
COM
Position
158
COM
Position
159
       

 

The Engineering EDR will contain Engineering Records, Imaging Status Records, Monitor Records, and Decommutation Map Records. The Decom Record is described in Appendix A. The Engineering record formats are shown in Figure B-2. Each of these records utilizes the Standard Record Header described in Appendix C, with some re-definitions noted below. The data block descriptions for Imaging appear in Table B-1.

 

Standard Header Redefinitions

 

For the Engineering Record, only the first 60 MF locations for the DPI fields will be used to flag the 60 EMF of the record. The remaining 20 locations and the GCI fields will be spares. The DQSE and GCI fields will be zeroed.

 

The Imaging Status Record will utilize the first 60 MF positions for DPI. DQSE and GCI fields will be zeroed. The first 4 MF locations for each field will flag GS MFs 1, 12, 21, and 31 of the 48-second science record from which the first ISS parameter set was extracted. The second 4 MF positions will flag the same MFs corresponding to the second set of parameters, etc.

 

10 BPS ENGINEERING RECORD FORMAT

 

The Engineering Record will be used in the Engineering EDR and all normal-rate Science EDR's excluding PWS. The Engineering Record Format is described in Figure B-4, the Standard Record Header in Appendix C, and the Engineering Data Block in Table B-3. This engineering data block contains engineering data for 60 EMF. Each channel will appear in the same location during this 48-minute record. Decommutation must be done with the last decom map preceding the Engineering Record.

 

The Engineering EDR will contain Engineering Records and Decommutation Map Records. The Decom Record is described in Appendix A. The record formats of the former two record types are shown in Figure B-2. Each of these records utilizes the Standard Record Header described in Appendix C, with some re-definitions noted below. The data block descriptions for these records appear in Figures B-2, B-4, B-6, and Tables B-1 and B-3.

 

Figure B-6. Engineering Record (965 32-bit Words)

 

Standard
Header
(60)
Subhdr
Spares
(15)
Engr
MF 1
(5)
Engr
MF 2
(15)
Engr
MF 3
(15)
Engr
MF 4
(15)
Engr
MF 5
(15). .
Engr
MF 59
. .(15)
Engr
MF 60
(15)
= 48 min
comprised of
150 CR6 MF

 

Standard Header Redefinitions

 

For the Engineering Record, only the first 60 MF locations for the DPI fields will be used to flag the 60 EMF of the record. The remaining 20 locations and the GCI fields will be spares. The DQSE and GCI fields will be zeroed.

 

 

Next: Appendix C

 

Return to EDR main page.

Return to Data File Descriptions 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.