Voyager Mission Operations Status Report #1198 – 13-19 October 2001
COMMAND TRANSMISSION & VERIFICATION OPERATIONS
Voyager 1 command operations consisted of the uplink of a command loss timer reset on 10/18 [DOY 291/0310z]. The command was not transmitted due to an antenna halt caused by an Az encoder problem at DSS-14 [DR G100432].
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 10/16 [DOY 289/1352z]. The spacecraft received four of the seven commands sent.
SEQUENCE GENERATION OPERATIONS
Started development of a mini-sequence for Voyager 2.
DATA RETURN OPERATIONS
Voyager 1 Data Processing and Operations:
There were 62.7 hours of DSN scheduled support for Voyager 1 of which 37.6 hours were large aperture coverage. There were no real-time or schedule support changes during the period.
There were two significant outages.ÊÊ The first outage of 0.6 hours duration on 10/18 [DOY 291] resulted from an antenna halt caused by Az encoder problems at DSS-14 [DR G100432]. The second outage of 2.2 hours duration on 10/19 [DOY 292] resulted from signal attenuation caused by rain at DSS-65 [DR L100211].Ê
Science instrument performance was nominal for all activities during this period. One frame of GS-4 data was recorded this week. Fifteen frames of data were played back on October 16, 97% of this data were recovered. Fourteen frames of data were played back on October 17, 94% of this data were recovered. The EDR backlog is 2 days.Voyager 2 Data Processing and Operations:
There were 63.5 hours of DSN scheduled support for Voyager 2 of which 38.1 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. One frame of GS-4 data was recorded this week. A second frame of GS-4 data was recorded on October 13, using the BHELI 1 cyclic, which was enabled on July 14. The EDR backlog is 2 days.
FLIGHT SYSTEM PERFORMANCE
Voyager 1 performance was nominal during this report period. Activities included switching X-Band to Hi Power on 10/15 (DOY 288), DTR PWS playback on 10/16 and 10/17 (DOY 289 and 291), and X-Band to Low power on 10/18 (DOY 289).
Voyager 2 performance was nominal during this report period. Activities included a PMPCAL on 10/16 (DOY 289) and the turning ON of Gyros A & B on 10/18 (DOY 291)
Spacecraft | Consumption One Week (Gm) | Propellant Remaining (Kg) | Output (Watts) | Margin (Watts) |
31 | 10.34 | 31.20 | 311.2 | 29 |
32 | 10.11 | 33.07 | 312.8 | 44 |
RANGE, VELOCITY AND ROUND TRIP LIGHT TIME AS OF 10/19/01
Voyager 1 | Voyager 2 | |
Distance from the Sun (Km) | 12,365,000,000 | 9,774,000,000 |
Distance from the Sun (Mi) | 7,683,000,000 | 6,074,000,000 |
Distance from the Earth (Km) | 12,451,000,000 | 9,796,000,000 |
Distance from the Earth (Mi) | 7,737,000,000 | 6,087,000,000 |
Total Distance Traveled Since Launch (Km) | 14,180,000,000 | 13,313,000,000 |
Total Distance Traveled Since Launch (Mi) | 8,811,000,000 | 8,273,000,000 |
Velocity Relative to Sun (Km/sec) | 17.241 | 15.737 |
Velocity Relative to Sun (Mi/hr) | 38,566 | 35,202 |
Velocity Relative to Earth (Km/sec) | 43.297 | 42.200 |
Velocity Relative to Earth (Mi/hr) | 96,853 | 94,397 |
Round Trip Light Time (Hours:Minutes:Seconds) | 23:04:26 | 18:09:18 |