ULYSSES MISSION OPERATIONS REPORT No. 984

PERIOD: 30th June 2009

Mission day 6843 - the final day !

 

 

1.       MISSION OPERATIONS

 

The Ulysses mission ended on 30th June 2009 with the following activities (all times are UTC):

 

Via the DSN 70m antenna at Canberra:

   181.06:45:00  DSS-43 BOT

   181.07:00:00  Switch EPC 1/2 off

   181.07:10:00  Switch off PAPS HV (-15/-30 KV)

   181.07:11:00  Switch off Deflection Plate Power Supply and GLG experiment heaters

   181.07:12:00  Disable MCP Power Supplies

   181.07:13:00  Switch off Detector Linear Channels

   181.07:20:00  Deschedule LOC Program

   181.07:25:00  Time-tagged command to switch off BAM-I HV (to execute at 181.16:15 SCET )

   181.07:30:00  Send time-tagged command for last Earth Pointing Manoeuvre

   181.08:50:00  DSS-43 EOT

  

While out of pass:

   181.11:20:11  SCET Open-loop slew manoeuvre X201

                        Spacecraft attitude to be Earth pointing at the mid-point of the next pass.

                        This was the final slew manoeuvre of the mission and used the same thruster (LA1) that was used for all Earth-pointing manoeuvres throughout the entire mission.

                       

Via the DSN 70m antenna at Madrid:

   181.15:35:00  DSS-63 BOT

   181.15:50:00  Time-tagged command  (to execute at 19:00 SCET)

                        RX 1 on, 64BPS ENG, TX2/RX2 to LGA/R, TX1/RX1 to LGA/F

   181.15:55:00  Time-tagged command  (to execute at 18:45 SCET)

                        AOCS configuration: open LV 2, ME-2 on, Sun Sensor gain to low, CE-1 off

   181.16:05:00  Switch off SIM KET HV1 off

   181.16:15:00  Switch on the X Wing Heaters

   181.16:20:00  Deschedule CONJ (ending fuel bleed manoeuvres)

   181.16:25:00  Switch off DSU

   181.16:30:00  Update Primary and Backup Tables

   181.16:45:00  Monitor final fuel bleed manoeuvre

   181.16:48:00  Switch off SIM KET HV2 off

   181.17:00:00  Monitor BAM-I HV off

   181:17:34:00 Monitor SIM KET HV1 off

   181.17:44:00  Monitor X Wing Heaters on

   181.17:49:00  Monitor CONJ descheduling

   181.17:54:00  Monitor DSU switch off

   181.17:59:00  Monitor the updating of PT and BT

   181.18:18:00  Monitor SIM KET HV2 off

   181.19:30:00  Monitor AOCS configuration changes

   181.19:45:00  Monitor RX 1 on

   181.19:52:00  64bps, some data collection at 64bps

   181.20:08:32  RFDU reconfiguration: Loss of signal

   181.20:15:00  Spacecraft S-band transmitter off

   181.20:20:00  DSS-63 EOT

 

 

The final data format received was at 09.181.19:24:26.751 spacecraft event time.

 

 

MANOEUVRES

 

Fuel bleeding was performed automatically every 2 hours throughout the final day using the onboard CONJ program. A command to deschedule CONJ was transmitted at 181.16:20 UTC and executed on-board the spacecraft at 17:04 UTC.

 

A final Earth-pointing open-loop slew executed at 181:11:20 spacecraft event time (SCET) to point the high gain antenna towards Earth during the final pass.

 

 

2.       SPACECRAFT STATUS

 

POWER

ATT/ORBIT

TELEMETRY/CMD

DATA HANDLING

THERMAL

Nominal
189 W

Nominal

S-Band Tx1
RX2 -118 dBm

Nominal

DSU1 in use

Nominal

 

 

 

DATE

BAM-I

GLG

GRU

HED

HUS

KEP

LAN

SIM

STO

30 Jun

HV Off

HV Off

Off

On

Off

Off

On

HV Off

Off

 

 

3.       FLIGHT DYNAMICS

 

DATE

SOLAR ASPECT

SUN-PROBE-EARTH

SPIN RATE

29 Jun

9.40°

9.26°

4.938 rpm

 

 


4.       ORBITAL DATA

 

DATA TAKEN AT

00:00:00 UTC 29 June 2009

DISTANCE FROM EARTH

             798,968,261 km

DISTANCE FROM SUN

             710,122,896 km

VELOCITY REL. TO EARTH

                   137,067 km/hour

VELOCITY REL. TO SUN

                     38,274 km/hour

ECLIPTIC LATITUDE

                       25.59 ° North

HELIOGRAPHIC LATITUDE

                       18.64 ° North

 

 

5.       GROUND SEGMENT

 

The final day's activities were scheduled to begin with a DSS-14 pass. However, the entire track was lost due to antenna problems. An additional pass from DSS-43 was obtained to perform preliminary decommissioning activities before the final DSS-63 track (thanks to the Voyager project for releasing antenna time on short notice).

 

DATE

GOLDSTONE

CANBERRA

MADRID

30 Jun

DSS-14

Unavailable due to antenna problems

DSS-43

Penultimate Pass

DSS-63

Final Pass

 

 

6.       PLANNED OPERATIONS

 

After more than 18 years of outstanding science return, the Ulysses mission ended on 30 June 2009. No further spacecraft operations are planned. Archiving activities will continue until 30 September.


Last signal from Ulysses via DSS-63:

 

 

 

Thanks to all those who have helped make Ulysses such a success.

 

Very best regards,

Nigel Angold