Voyager Mission Operations Status Report # 2011-11-04, Week Ending
November 4, 2011
Command
Transmission & Verification Operations
There
were no command operations in support of Voyager 1 during the period.
Voyager 2 command operations consisted of the uplink of a Command
Loss Timer Reset and CCSL B154A on 11/04 [DOY 308/1050z]. The spacecraft received all commands sent and
the CCSL was verified.
Sequence
Generation Operations
Began sequence development of CCSL B154B.
Data Return
Operations
Voyager 1 Data Processing and Operations:
There were 45.4 hours of DSN scheduled support for Voyager 1 of
which 45.4 hours were large aperture coverage. There was one real-time support
change on 10/03 [DOY 303] when DSS-25 supported 1.4 hours in place of DSS-14
down due to a Red Antenna [DR G112088].
The total actual support for the period was 45.4 hours of which 44.0
hours were large aperture coverage.
There was one significant outage of 5.1 hours on 10/03 [DOY 303]
due to a Red Antenna at DSS-14 [DR G112088].
Science instrument performance was
nominal for all activities during this period.
One frame of GS-4 data was recorded this week. A second frame of GS-4 data was recorded on
November 1. The EDR backlog is 3 days.
Voyager 2 Data Processing and Operations:
There were 37.1 hours of DSN
scheduled support for Voyager 2 of which 22.1 hours were large aperture
coverage. There were no real-time or
schedule support changes made or significant outages during the period.
Science
instrument performance was nominal for all activities during this period. The EDR backlog is 2 days.
Flight System
Performance
Voyager 1 performance was nominal during this report period. Activities included 1 LECP observation on
1/29 (DOY 302), 2 LECP observations on 10/30 (DOY 303), 1 LECP observation on
10/31 (DOY 305), an ASCAL on 11/1 (DOY 305), and 1 LECP observation on 11/2
(DOY 306), and 11/3 (DOY 307).
Voyager 2 performance was nominal during this report period.
PROPELLANT/POWER
CONSUMABLES STATUS AS OF THIS REPORT
|
Spacecraft |
Consumption One Week
(Gm) |
Propellant Remaining
(Kg) |
Output (Watts) |
Margin (Watts) |
|
1 |
263.12* |
24.10 |
267.7 |
10 |
|
2 |
4.66 |
27.08 |
268.9 |
28 |
*1
ASCAL and 5 LECP Observations
RANGE,
VELOCITY AND ROUND TRIP LIGHT TIME AS OF THIS REPORT
|
|
Voyager 1 |
Voyager 2 |
|
Distance from the Sun (Km) |
17,767,000,000 |
14,488,000,000 |
|
Distance from the Sun (Mi) |
11,040,000,000 |
9,002,000,000
|
|
Distance from the Earth (Km) |
17,869,000,000 |
14,534,000,000 |
|
Distance from the Earth (Mi) |
11,103,00,000 |
9,031,000,000 |
|
Total Distance Traveled Since Launch (Km) |
23,563,000,000 |
22,507,000,000 |
|
Total Distance Traveled Since Launch (Mi) |
14,641,000,000 |
13,985,000,000 |
|
Velocity Relative to Sun
(Km/sec) |
17.051 |
15.656 |
|
Velocity Relative to Sun
(Mi/hr) |
38,141 |
34,566 |
|
Velocity Relative to Earth
(Km/sec) |
41.497 |
41.656 |
|
Velocity Relative to Earth
(Mi/hr) |
92,825 |
93,182 |
|
Round Trip Light Time (hh:mm:ss) |
33:05:56 |
26:56:02 |