ACE Weekly 08/22/03 - 08/28/03 All ACE spacecraft subsystems are performing nominally. An attitude maneuver was successfully executed on 08/27/03. The next attitude maneuver is scheduled for 09/02/03. ============================================================================ Orbit Events: The next SEV transit will occur during the 09/01/03 - 09/23/03 time frame. Expected minimum SEV angle will be 1.76 degrees. The essential timeline based on a 30-min step scan for this 22 day, 8.5 hour event is: - SEZ entry (4.75 deg inbound) on Sept. 1 at 0100Z - Minimum Sun-Earth-ACE angle = 1.760 deg on Sept. 12 at 0800Z - SEZ exit (4.75 deg outbound) on Sept. 23 at 0930Z ===================================================================== OCRs Executed: NONE ===================================================================== Ongoing Activities: TAPS: Trending, Analysis and Plotting System (TAPS) development continues with emphasis being placed on fixing the DRs attributed to prior releases. Release 4.1.6 was installed successfully on 08/05/03 and is currently in test by FOT. Release 4.1.7 is tentatively scheduled for installation during the week of 09/01/03. ---------------------------------------------------------------------------- Automation (ROBOTT): - Offline testing is progressing well on String 2. There are a few minor issues, but nothing that is keeping the system from running nominally. We expect to be finished testing this new release on String 2 by the end of September. - FOT currently training on the Automation system. - Automation Team testing of HSM and Command & Control on String 3 has resumed, delivery date to FOT is still TBD. ---------------------------------------------------------------------------- NSP Demo: An NSP Demo with DSS-24 was performed successfully on DOY 238 (08/26/03). All 3 bit rates were acquired (498, 7968 & 87648bps) and 33 commands were transmitted to the spacecraft. The Ground Receipt Time (GRT) was good and within 10 milliseconds of our earlier pass with DSS-16. No data corruption was found. ===================================================================== Anomalies: DOY 03237 (08/25/2003) ACE Anomaly G03-0078 - GDS 34m (DSS-24) Telemetry Offline Loss of telemetry from DSS-24 from 16:09:37 - 16:17:54 due to TLP4 (Telemetry Processor 4) problem. IMPACT: Delayed pass activities. All telemetry was subsequently recovered. DR# G103249 ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~ Glen A. Miller ACE Flight Operations Observatory Engineer Honeywell Technology Solutions Inc. Goddard Space Flight Center Building 14, Room W10A Mail Stop 428.2 Greenbelt, MD 20771 Office: 301-286-7071 Pager: 800-425-3174 Fax: 301-286-1729 Email: gamiller@pop500.gsfc.nasa.gov ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~