Voyager Mission Operations Status
Report # 2012-08-03, Week Ending August 3, 2012
Command Transmission
& Verification Operations
Voyager
1 command operations consisted of the uplink of a Command Loss Timer Reset on 07/30
[DOY 212/2250z]. The spacecraft received
the command.
Voyager
2 command operations consisted of the uplink of seven bracketed Command Loss
Timer Resets sent on five-minute centers using 0.5 Hz steps on 08/02 [DOY 215/1427z].
The spacecraft received two of the seven commands sent.
Sequence Generation Operations
Data Return Operations
Voyager
1 Data Processing and Operations:
There
were 57.0 hours of DSN scheduled support for Voyager 1 of which 49.8 hours were
large aperture coverage. There were no real-time or schedule support changes
made during the period.
There was one significant outage of
0.7 hours on 08/01 [DOY 214] due to rain at DSS-14 [DR G113069].
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 August 3. The EDR backlog is
6 days.
Voyager
2 Data Processing and Operations:
There were 52.8 hours of DSN scheduled support for
Voyager 2 of which 44.9 hours were large aperture coverage. There were no real-time or schedule support
changes made or significant outages during the period.
Voyager
1 performance was nominal during this report period. Activities included switching to X-Band high
power and execution of a MAGROL on 7/23 (DOY 206), and LECP observations on
7/24 (DOY 207, 7/25 (DOY 208), and 7/26 (DOY 209).
Science instrument performance was nominal for all
activities during this period. The EDR
backlog is 7 days.
Flight System Performance
Voyager
1 performance was nominal during this report period. Activities included LECP Observations 7/29
(DOY 212), 7/30 (DOY 213), 7/31 (DOY 214), 8/1 (DOY 215), and 8/2 (DOY 216)
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 |
275.80* |
22.42 |
264.5 |
11 |
|
2 |
4.36 |
26.72 |
265.7 |
31 |
*LECP
Observations 2012/211, 212, 213, 214, 215, 216
RANGE, VELOCITY AND ROUND TRIP LIGHT
TIME AS OF THIS REPORT
|
|
Voyager 1 |
Voyager 2 |
|
Distance
from the Sun (Km) |
18,167,000,000 |
14,841,000,000 |
|
Distance
from the Sun (Mi) |
11,289,000,000 |
9,222,000,000 |
|
Distance
from the Earth (Km) |
18,098,000,000 |
14,725,000,000 |
|
Distance
from the Earth (Mi) |
11,246,000,000 |
9,149,000,000 |
|
Total
Distance Traveled Since Launch (Km) |
24,260,000,000 |
23,224,000,000 |
|
Total
Distance Traveled Since Launch (Mi) |
15,075,000,000 |
14,431,000,000 |
|
Velocity
Relative to Sun (Km/sec) |
17.045 |
15.440 |
|
Velocity
Relative to Sun (Mi/hr) |
38,127 |
34,537 |
|
Velocity
Relative to Earth (Km/sec) |
42.130 |
35.754 |
|
Velocity
Relative to Earth (Mi/hr) |
94,241 |
79,979 |
|
Round
Trip Light Time (hh:mm:ss) |
33:31:28 |
27:17:08 |