MISSION_NAME = "CASSINI" SPACECRAFT_NAME = "CASSINI" DATA_SET_ID = "SPICE_SPK_FILE" KERNEL_TYPE_ID = "SPK" PRODUCT_ID = "081111AP_SCPSE_08316_08331.xsp" PRODUCT_CREATION_TIME = 2008-11-11T11:06:09 PRODUCER_ID = "CASSINI_NAV" MISSION_PHASE_NAME = "TOUR" PRODUCT_VERSION_TYPE = "PREDICT" PLATFORM_OR_MOUNTING_NAME = "N/A" START_TIME = 2008-11-10T10:07:55 STOP_TIME = 2008-11-26T11:58:55 SPACECRAFT_CLOCK_START_COUNT = "N/A" SPACECRAFT_CLOCK_STOP_COUNT = "N/A" TARGET_NAME = { "CASSINI", "MERCURY BARYCENTER", "VENUS BARYCENTER", "EARTH BARYCENTER", "MARS BARYCENTER", "JUPITER BARYCENTER", "SATURN BARYCENTER", "URANUS BARYCENTER", "NEPTUNE BARYCENTER", "PLUTO BARYCENTER", "SUN", "MERCURY", "VENUS", "MOON", "EARTH", "MARS", "MIMAS", "ENCELADUS", "TETHYS", "DIONE", "RHEA", "TITAN", "HYPERION", "IAPETUS", "PHOEBE", "SATURN" } INSTRUMENT_NAME = "N/A" INSTRUMENT_ID = "N/A" SOURCE_PRODUCT_ID = "SEE COMMENTS" NOTE = "SPICE transfer format SPK file." ; ap_scpse.bsp LOG FILE ; ; Created 2008-11-11/11:05:48.00. ; ; BEGIN NIOSPK COMMANDS LEAPSECONDS_FILE = /cnav/inputs/naif/latest.tls SPK_FILE = ap_scpse.bsp INCLUDE_TEXT_FILE = spk_comments_ap_scpse.txt INCLUDE_TEXT_FILE = Readme SOURCE_NIO_FILE = /cnav/Man/working/MAS/offline/prime/O171_g/p_with_mvr.nio BODIES = -82 BEGIN_TIME = CAL-ET 2008 NOV 10 10:08:59.898 END_TIME = CAL-ET 2008 NOV 26 12:00:00.000 SOURCE_NIO_FILE = /cnav/OD/deliveries/081111_091T47/peph.nio BEGIN_TIME = CAL-ET 2008 NOV 10 10:08:59.898 END_TIME = CAL-ET 2008 NOV 26 12:00:00.000 SOURCE_NIO_FILE = /cnav/OD/deliveries/081111_091T47/seph.nio BEGIN_TIME = CAL-ET 2008 NOV 10 10:08:59.898 END_TIME = CAL-ET 2008 NOV 26 12:00:00.000 ; END NIOSPK COMMANDS % template version $Revision: 1.14 $ $Date: 2006/08/18 20:07:29 $ - - For OTM-171 based upon OD solution 081111_091T47. This file is invalid after 26-NOV-2008 12:00:00.0000 ET or execution of subsequent maneuvers. This file accounts for maneuvers up to and including OTM-171. This file includes planetary and satellite ephemerides. - FILENAME: 081111AP_SCPSE_08316_08331.BSP PURPOSE OF DELIVERY: OTM-171 (MAS ID O171_g) DELIVERY DATE: 081111 PLANETARY EPHEMERIS USED: from OD delivery SATELLITE/ASTEROID/ROCK EPHEMERIS USED: from OD delivery START EPOCH OF FILE: 10-NOV-2008 10:08:59.9 ET SCET END EPOCH OF FILE: 26-NOV-2008 12:00:00.0000 ET SCET ------ COMMENTS FROM NAV/MVR FOR OTM-171 O171_g By: Cassini-Huygens Navigation Team Profile file: MPF_O171_g_081111_091T47 Maneuver Start: 12-NOV-2008 22:09:00.000 UTC SCET ------ COMMENTS FROM NAV/OD FOR DELIVERY 081111_091T47 -------------------------------------------------------------------------------- DELIVERY NAME: 081111_091T47 BY: Kevin Criddle DATE: November 11, 2008 PURPOSE OF DELIVERY: Final OTM171 OD Delivery ORIGINAL DIRECTORY: /cnav/OD/ops/091T47/epoch_081020/otm171/081111 case 8 COMMENTS: Epoch of arc is 20-OCT-2008 18:00:00.000000000 Spacecraft a priori state and covariance from sat301 delivery Spacecraft State covariance with scale factor of 5 Satellite/planet Covariance sat301 2-way Doppler and Range through 11-NOV-2008 17:30 Optical Data through 11-NOV-2008 09:25 Weights by pass for F2 and SRA SMALL FORCES: SMFDV001 22-OCT-2008 10:01:15.8 SMFDV002 23-OCT-2008 17:15:02.7 SMFDV003 24-OCT-2008 10:18:35.0 SMFDV004 24-OCT-2008 16:37:53.6 SMFDV005 25-OCT-2008 17:15:55.3 SMFDV006 26-OCT-2008 09:48:45.8 SMFDV007 27-OCT-2008 09:40:42.5 SMFDV008 28-OCT-2008 16:32:26.3 SMFDV009 30-OCT-2008 16:35:38.5 SMFDV010 01-NOV-2008 16:15:19.2 SMFDV011 03-NOV-2008 14:16:09.0 SMFDV012 03-NOV-2008 19:11:50.1 SMFDV013 06-NOV-2008 08:51:06.2 SMFDV014 07-NOV-2008 13:36:29.3 SMFDV015 08-NOV-2008 21:37:28.6 SMFDV016 08-NOV-2008 23:22:57.3 SMFDV017 09-NOV-2008 00:01:45.4 SMFDV018 09-NOV-2008 15:45:19.5 MANEUVERS OTM169 RCS 0.225 m/s 29-Oct-2008 (telemetry a priori and sigmas for pointing) OTM170 ME 9.10 m/s 08-NOV-2008 (design a priori values and sigmas for pointing) NOTES OTM169 was an underburn of approximately 7.0 mm/s, or 5.2 sigma. 2-way Doppler and Range through 11-NOV-2008 17:30 available until the next day. The post-burn spinup and redundant background sequence bias immediately following the burn was replaced with a priori values based on telemetry and assuming a 5% a prior uncertainty in magnitude. ------------------------------------------------------------------------------------- \beginlabel MISSION_NAME = "CASSINI" SPACECRAFT_NAME = "CASSINI" DATA_SET_ID = "SPICE_SPK_FILE" KERNEL_TYPE_ID = "SPK" PRODUCT_ID = "081111AP_SCPSE_08316_08331.xsp" PRODUCT_CREATION_TIME = 2008-11-11T11:06:09 PRODUCER_ID = "CASSINI_NAV" MISSION_PHASE_NAME = "TOUR" PRODUCT_VERSION_TYPE = "PREDICT" PLATFORM_OR_MOUNTING_NAME = "N/A" START_TIME = 2008-11-10T10:07:55 STOP_TIME = 2008-11-26T11:58:55 SPACECRAFT_CLOCK_START_COUNT = "N/A" SPACECRAFT_CLOCK_STOP_COUNT = "N/A" TARGET_NAME = { "CASSINI", "MERCURY BARYCENTER", "VENUS BARYCENTER", "EARTH BARYCENTER", "MARS BARYCENTER", "JUPITER BARYCENTER", "SATURN BARYCENTER", "URANUS BARYCENTER", "NEPTUNE BARYCENTER", "PLUTO BARYCENTER", "SUN", "MERCURY", "VENUS", "MOON", "EARTH", "MARS", "MIMAS", "ENCELADUS", "TETHYS", "DIONE", "RHEA", "TITAN", "HYPERION", "IAPETUS", "PHOEBE", "SATURN" } INSTRUMENT_NAME = "N/A" INSTRUMENT_ID = "N/A" SOURCE_PRODUCT_ID = "SEE COMMENTS" NOTE = "SPICE transfer format SPK file." \endlabel Brief. Version: 2.2.0 (SPICE Toolkit N0058) Summary for: 081111AP_SCPSE_08316_08331.bsp Bodies Start of Interval (ET) End of Interval (ET) ------- ----------------------------- ----------------------------- -82 CASSINI 2008 NOV 10 10:08:59.899 2008 NOV 26 12:00:00.000 1 MERCURY BARYCENTER Same coverage as previous object 2 VENUS BARYCENTER Same coverage as previous object 3 EARTH BARYCENTER Same coverage as previous object 4 MARS BARYCENTER Same coverage as previous object 5 JUPITER BARYCENTER Same coverage as previous object 6 SATURN BARYCENTER Same coverage as previous object 7 URANUS BARYCENTER Same coverage as previous object 8 NEPTUNE BARYCENTER Same coverage as previous object 9 PLUTO BARYCENTER Same coverage as previous object 10 SUN Same coverage as previous object 199 MERCURY Same coverage as previous object 299 VENUS Same coverage as previous object 301 MOON Same coverage as previous object 399 EARTH Same coverage as previous object 499 MARS Same coverage as previous object 601 MIMAS Same coverage as previous object 602 ENCELADUS Same coverage as previous object 603 TETHYS Same coverage as previous object 604 DIONE Same coverage as previous object 605 RHEA Same coverage as previous object 606 TITAN Same coverage as previous object 607 HYPERION Same coverage as previous object 608 IAPETUS Same coverage as previous object 609 PHOEBE Same coverage as previous object 699 SATURN Same coverage as previous object