MISSION_NAME = "CASSINI" SPACECRAFT_NAME = "CASSINI" DATA_SET_ID = "SPICE_SPK_FILE" KERNEL_TYPE_ID = "SPK" PRODUCT_ID = "051122AP_SCPSE_05326_05333.xsp" PRODUCT_CREATION_TIME = 2005-11-22T11:35:40 PRODUCER_ID = "CASSINI_NAV" MISSION_PHASE_NAME = "TOUR" PRODUCT_VERSION_TYPE = "PREDICT" PLATFORM_OR_MOUNTING_NAME = "N/A" START_TIME = 2005-11-22T11:29:02 STOP_TIME = 2005-11-29T22:37:39 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 2005-11-22/11:35:31.00. ; ; 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/O043_i/p_with_mvr.nio BODIES = -82 BEGIN_TIME = CAL-ET 2005 NOV 22 11:30:06.000 END_TIME = CAL-ET 2005 NOV 29 22:38:43.000 SOURCE_NIO_FILE = /cnav/OD/deliveries/051122_018R1/peph.nio BEGIN_TIME = CAL-ET 2005 NOV 22 11:30:06.000 END_TIME = CAL-ET 2005 NOV 29 22:38:43.000 SOURCE_NIO_FILE = /cnav/OD/deliveries/051122_018R1/seph.nio BEGIN_TIME = CAL-ET 2005 NOV 22 11:30:06.000 END_TIME = CAL-ET 2005 NOV 29 22:38:43.000 ; END NIOSPK COMMANDS % template version $Revision: 1.12 $ $Date: 2005/11/15 15:49:49 $ - - For OTM-043 based upon OD solution 051122_018R1. This file is invalid after 29-NOV-2005 22:38:43.0 UTC or execution of subsequent maneuvers. This file accounts for maneuvers up to and including OTM-043. This file includes planetary and satellite ephemerides. - FILENAME: 051122AP_SCPSE_05326_05333.BSP PURPOSE OF DELIVERY: OTM-043 (MAS ID O043_i) DELIVERY DATE: 051122 PLANETARY EPHEMERIS USED: from OD delivery SATELLITE/ASTEROID/ROCK EPHEMERIS USED: from OD delivery START EPOCH OF FILE: 22-NOV-2005 11:30:06.0 UTC SCET END EPOCH OF FILE: 29-NOV-2005 22:38:43.0 UTC SCET ------ COMMENTS FROM NAV/MVR FOR OTM-043 O043_i By: Cassini-Huygens Navigation Team Profile file: MPF_O043_i_051122_018R1 Maneuver Start: 23-NOV-2005 13:03:00.000 UTC SCET ------ COMMENTS FROM NAV/OD FOR DELIVERY 051122_018R1 -------------------------------------------------------------------------------- DELIVERY NAME: 051122_018R1 BY: Frederic Pelletier DATE: November 22, 2005 PURPOSE OF DELIVERY: Final OTM043 OD Delivery ORIGINAL DIRECTORY: /cnav/OD/ops/018R1/otm043/epoch_051020/051122 case 11 COMMENTS: Epoch of arc is October 20, 2005 06:00 ET Spacecraft a priori state and covariance from sat226 delivery Spacecraft State covariance with scale factor of 5 Satellite/planet Covariance sat226 2-way Doppler and Range through 22-NOV-2005 16:56 Optical Data through 21-NOV-2005 17:38 Weights by pass for F2 and SRA F1 and F3 data used on 2005/10/21 T8 RCS Activity based on Telemetry using GLAR approximation Mass decrement on 31-OCT to match OTM041 mapdf Mass decrement on 13-Nov to match OTM042 mapdf Mass decrement on 23-Nov to match OTM043 mapdf Entire DSS 25 F2 Pass on doy 321 deleted Entire DSS 25 F2 Pass on doy 322 deleted SMALL FORCES SMFDV322', # 2005-10-21 15:52:28.625000 SMFDV323', # 2005-10-28 02:33:09.250000 SMFDV324', # 2005-10-28 03:53:38.613999 SMFDV325', # 2005-10-28 04:33:22.599000 SMFDV326', # 2005-10-28 05:37:39 SMFDV327', # 2005-10-29 06:13:35 SMFDV328', # 2005-10-31 13:25:09.625000 SMFDV329', # 2005-10-31 14:50:39.250000 SMFDV330', # 2005-11-04 16:25:50 SMFDV331', # 2005-11-04 16:51:24 SMFDV332', # 2005-11-10 14:16:00 SMFDV333', # 2005-11-13 13:31:03.625000 SMFDV334', # 2005-11-13 14:30:38.125000 MANEUVERS OTM039 - DV, RA, Dec, and Start Time OTM041 - DV, RA, Dec, and Start Time OTM042 - DV, RA, Dec, and Start Time ------------------------------------------------------------------------------------- \beginlabel MISSION_NAME = "CASSINI" SPACECRAFT_NAME = "CASSINI" DATA_SET_ID = "SPICE_SPK_FILE" KERNEL_TYPE_ID = "SPK" PRODUCT_ID = "051122AP_SCPSE_05326_05333.xsp" PRODUCT_CREATION_TIME = 2005-11-22T11:35:40 PRODUCER_ID = "CASSINI_NAV" MISSION_PHASE_NAME = "TOUR" PRODUCT_VERSION_TYPE = "PREDICT" PLATFORM_OR_MOUNTING_NAME = "N/A" START_TIME = 2005-11-22T11:29:02 STOP_TIME = 2005-11-29T22:37:39 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: 051122AP_SCPSE_05326_05333.bsp Bodies Start of Interval (ET) End of Interval (ET) ------- ----------------------------- ----------------------------- -82 CASSINI 2005 NOV 22 11:30:06.000 2005 NOV 29 22:38:43.000 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