MISSION_NAME = "CASSINI" SPACECRAFT_NAME = "CASSINI" DATA_SET_ID = "SPICE_SPK_FILE" KERNEL_TYPE_ID = "SPK" PRODUCT_ID = "100629AP_SCPSE_10169_10192.xsp" PRODUCT_CREATION_TIME = 2010-06-29T09:15:39 PRODUCER_ID = "CASSINI_NAV" MISSION_PHASE_NAME = "TOUR" PRODUCT_VERSION_TYPE = "PREDICT" PLATFORM_OR_MOUNTING_NAME = "N/A" START_TIME = 2010-06-18T07:02:40 STOP_TIME = 2010-07-11T19:58:55 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 2010-06-29/09:15:25.00. ; ; 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/O255_b/p_with_mvr.nio BODIES = -82 BEGIN_TIME = CAL-ET 2010 JUN 18 07:03:45.000 END_TIME = CAL-ET 2010 JUL 11 20:00:00.000 SOURCE_NIO_FILE = /cnav/OD/deliveries/100628a_134T71/peph.nio BEGIN_TIME = CAL-ET 2010 JUN 18 07:03:45.000 END_TIME = CAL-ET 2010 JUL 11 20:00:00.000 SOURCE_NIO_FILE = /cnav/OD/deliveries/100628a_134T71/seph.nio BEGIN_TIME = CAL-ET 2010 JUN 18 07:03:45.000 END_TIME = CAL-ET 2010 JUL 11 20:00:00.000 ; END NIOSPK COMMANDS % template version $Revision: 1.14 $ $Date: 2006/08/18 20:07:29 $ - - For OTM-255 based upon OD solution 100628a_134T71. This file is invalid after 11-JUL-2010 20:00:00 ET or execution of subsequent maneuvers. This file accounts for maneuvers up to and including OTM-255. This file includes planetary and satellite ephemerides. - FILENAME: 100629AP_SCPSE_10169_10192.BSP PURPOSE OF DELIVERY: OTM-255 (MAS ID O255_b) DELIVERY DATE: 100629 PLANETARY EPHEMERIS USED: from OD delivery SATELLITE/ASTEROID/ROCK EPHEMERIS USED: from OD delivery START EPOCH OF FILE: 18-JUN-2010 07:03:45 ET SCET END EPOCH OF FILE: 11-JUL-2010 20:00:00 ET SCET ------ COMMENTS FROM NAV/MVR FOR OTM-255 O255_b By: Cassini-Huygens Navigation Team Profile file: MPF_O255_b_100628a_134T71 Maneuver Start: 30-JUN-2010 07:40:00.000 UTC SCET ------ COMMENTS FROM NAV/OD FOR DELIVERY 100628a_134T71 -------------------------------------------------------------------------------- DELIVERY NAME: 100628a_134T71 BY: Rodica Ionasescu DATE: June 29, 2010 PURPOSE OF DELIVERY: Final Delivery for OTM255 ORIGINAL DIRECTORY: /cnav/OD/ops/134T71/epoch_100613/otm255/100628a case 4 COMMENTS: Epoch of arc is Spacecraft a priori state and covariance from previous arc Spacecraft State covariance with scale factor of 10 Satellite/planet Covariance based on sat335 2-way Doppler and Range through 28-JUN-2010 22:17 Optical Data through 02-JUN-2010 23:35 Weights by pass for F2 and SRA T70 RCS activity modeled with telemetry data SMALL FORCES: SMFDV001 14-JUN-2010 10:20:30.8 SMFDV002 20-JUN-2010 00:58:10.6 SMFDV004 21-JUN-2010 02:03:09.5 SMFDV005 24-JUN-2010 07:18:44.0 SMFDV006 24-JUN-2010 08:44:08.8 SMFDV007 24-JUN-2010 09:27:41.8 SMFDV008 25-JUN-2010 19:45:39.0 MANEUVERS OTM253 RCS 0.025 m/s 18-JUN-2010 02:11:00 OTM254 ME 0.874 m/s 24-JUN-2010 07:56:08 ------------------------------------------------------------------------------------- \beginlabel MISSION_NAME = "CASSINI" SPACECRAFT_NAME = "CASSINI" DATA_SET_ID = "SPICE_SPK_FILE" KERNEL_TYPE_ID = "SPK" PRODUCT_ID = "100629AP_SCPSE_10169_10192.xsp" PRODUCT_CREATION_TIME = 2010-06-29T09:15:39 PRODUCER_ID = "CASSINI_NAV" MISSION_PHASE_NAME = "TOUR" PRODUCT_VERSION_TYPE = "PREDICT" PLATFORM_OR_MOUNTING_NAME = "N/A" START_TIME = 2010-06-18T07:02:40 STOP_TIME = 2010-07-11T19:58:55 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: 100629AP_SCPSE_10169_10192.bsp Bodies Start of Interval (ET) End of Interval (ET) ------- ----------------------------- ----------------------------- -82 CASSINI 2010 JUN 18 07:03:45.000 2010 JUL 11 20:00:00.000 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