ACE Weekly 09/02/05 - 09/08/05 All ACE spacecraft subsystems are performing nominally. ============================================================================ Orbit/Attitude: Type Attitude Attitude Date 09/07/05 09/07/05 DOY 250 2005 250 2005 Thrusters 2R 4R+ 4R- 2R 4R+ 4R- Duration 4:46 min 6:52 min Start Time 17:12:27z 18:07:39z Stop Time 17:17:13z 18:14:31z Firing 25 pulses 35 pulses The next attitude maneuver is scheduled for Friday 09/16/05. ============================================================================ OCRs: SWPX-040 is scheduled for Monday 09/12/05. The SWEPAM-E CEM High Voltage will be increased from level 14 to level 15 in order to compensate for sensor gain losses due to aging affects. ============================================================================ Ongoing Activities: Space Link Extension (SLE) - The schedule for the next DSN/Developer test with DTF-21 will be determined next week. ============================================================================ Extra Activities: DOY 249 (09/06/05) - TAPS release 4.4 was delivered and installed. This release resolved CDSID#21044 (incorrect data decommutation in ADC) but does not fix CDSID#21043 (1-second data gaps every 429 seconds). DOY 250 (09/07/05) - A 1-hour (2035-2135z) Project Interface Test (PIT) was completed for the equipment upgrade at DSS-27 (V5.9). We were informed that DSN's current setup does not correctly account for ground delays when generating the range data which causes an error of approximately 150 nanoseconds. DSN expects to have new software to correct the problem in January 2005. Also, during the test, DSS-27 stopped tracking after conscan was enabled (DR G106037). Further post-pass data analysis is underway. ============================================================================ Anomalies: DOY 247 (09/04/05) ACE Anomaly G05-0110 26m DSS-16 Antenna Pointing Problems Problems with the Metric Pointing Assembly (MPA) at Beginning Of Track (BOT) were resolved by the ground station with an equipment reboot. DR G106025 IMPACT: Activities delay 16 minutes. DOY 248 (09/05/05) ACE Anomaly G05-0111 ROBOTT/CC Failure Not Cleared ROBOTT generated a "Task Verification Failed" message due to a known problem (CDSID 21261). However, the failure was not cleared until later in the pass when a second procedure was being executed. IMPACT: Troubleshooting completed to ensure that the second procedure did not have failures. DOY 237 (08/25/05) ACE Anomaly G05-0112 26m 0158 TCP Data Unavailable Post pass analysis of the LMP PIT (DOY 237) shows that DSN's 0158 Monitor Data only provides data for 1 TCP. The station switches TCPs for each bit rate change. When the other TCP is used, the 0158 still gives data for the first TCP. Analysis of previous data shows that this problem has been occurring before the new LMP. IMPACT: Monitor data (including ground SNR) unavailable for trending and anomaly trouble-shooting. DOY 250 (09/07/05) ACE Anomaly S05-0036 S3DPU Limit Violations S3DPU_CONV_SEC_I had 1 brief red high limit violation (>440mA). SSDIDLECTR was 60-67. Increased solar activity started on DOY 250. Mark Popecki notified. 2005-250 16:22:30 - 16:22:32z 462 - 470mA IMPACT: S3DPU is expected to use more current during increased activity. DOY 250 (09/07/05) ACE Anomaly G05-0113 26m DSS-16 Ranging Cals Station unable to perform pre pass range cals due to problems with enabling pre pass ranging signals. DR G106033 IMPACT: Post pass range cals performed at the end of the support. DOY 250 (09/07/05) ACE Anomaly G05-0014 26m DSS-16 Signal Acquisition Station unable to acquire spacecraft downlink after earlier problems with pre pass range cals. DR G106034 IMPACT: Activities delayed 30 minutes. Gaps in playback data captured on DOY 251. DOY 250 (09/07/05) ACE Anomaly G05-0015 26m DSS-16 CMD Mod Index Station's CMD MIL changed during the troubleshooting of earlier downlink acquisition problems. Station unable to change value during support. Post pass analysis indicated a CMD Mod Index of 1.74rad/8.52dB as compared to the nominal value of 0.86rad/1.69dB. DR G106036 IMPACT: Uplink to spacecraft reduced with increased CMD Mod Index