Voyager Mission Operations Status Report # 2009-07-31,  Week Ending  July 31, 2009

 

Command Transmission & Verification Operations

 

Voyager 1 command operations consisted of the uplink of a Command Loss Timer Reset on 07/30 [DOY 211/2130z].  The spacecraft received the command.

 

Voyager 2 command operations consisted of the uplink of two HPOINT PTR DMROs and a Command Loss Timer Reset on 07/26 [DOY 207/1143z]. The spacecraft received all commands sent and both DMROs  were verified.

 

Sequence Generation Operations

 

Continue sequence development of CCSL B145.

 

Data Return Operations

 

Voyager 1 Data Processing and Operations:

 

There were 94.3 hours of DSN scheduled support for Voyager 1 of which 47.5 hours were large aperture coverage. There was one schedule support change on 07/25 [DOY 206] when 0.8 hours of DSS-63 support was released.  The total actual support was 93.5 hours of which 46.7 hours were large aperture coverage.  There were no significant outages during the period. 

 

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 July 31.  The EDR backlog is 2 day.

 

Voyager 2 Data Processing and Operations:

 

There were 70.5 hours of DSN scheduled support for Voyager 2 of which 35.2 hours were large aperture coverage. There were no real-time or schedule support changes made during the period.

 

There was one significant outage of 1.0 hours on 07/30 [DOY 211] due to a Comm. problem at ERNS1 [DR N105435].

 

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.  Activity included turning on the AB gyros on 7/31 [DOY 213].

 

Voyager 2 performance was nominal during this report period.  Activity included a PMPCAL on 7/28 [DOY 209].

 

PROPELLANT/POWER CONSUMABLES STATUS AS OF THIS REPORT

 

 

Spacecraft

Consumption

One Week (Gm)

Propellant

Remaining (Kg)

Output

(Watts)

Margin

(Watts)

1

4.85

26.61

277.0

33

2

5.10

28.26

278.3

32

 

 

RANGE, VELOCITY AND ROUND TRIP LIGHT TIME AS OF 7/31/2009

 

 

Voyager 1

Voyager 2

Distance from the Sun (Km)

16,555,000,000

13,420,000,000

Distance from the Sun (Mi)

10,287,000,000

8,339,000,000

Distance from the Earth (Km)

16,481,000,000

13,300,000,000

Distance from the Earth (Mi)

10,241,000,000

8,264,000,000

Total Distance Traveled Since Launch (Km)

21,111,000,000

20,103,000,000

Total Distance Traveled Since Launch (Mi)

13,118,000,000

12,491,000,000

Velocity Relative to Sun  (Km/sec)

17.082

15.504

Velocity Relative to Sun  (Mi/hr)

38,210

34,681

Velocity Relative to Earth  (Km/sec)

41.799

35.331

Velocity Relative to Earth  (Mi/hr)

93,502

79,032

Round Trip Light Time (hh:mm:ss)

30:31:48

24:38:44