MISSION_NAME = "CASSINI" SPACECRAFT_NAME = "CASSINI" DATA_SET_ID = "SPICE_SPK_FILE" KERNEL_TYPE_ID = "SPK" PRODUCT_ID = "050102AP_PE_05002_05017.xsp" PRODUCT_CREATION_TIME = 2005-01-02T15:24:49 PRODUCER_ID = "CASSINI_NAV" MISSION_PHASE_NAME = "TOUR" PRODUCT_VERSION_TYPE = "PREDICT" PLATFORM_OR_MOUNTING_NAME = "N/A" START_TIME = 2005-01-02T15:22:06 STOP_TIME = 2005-01-17T11:13:00 SPACECRAFT_CLOCK_START_COUNT = "N/A" SPACECRAFT_CLOCK_STOP_COUNT = "N/A" TARGET_NAME = { "MERCURY BARYCENTER", "VENUS BARYCENTER", "EARTH BARYCENTER", "MARS BARYCENTER", "JUPITER BARYCENTER", "SATURN BARYCENTER", "URANUS BARYCENTER", "NEPTUNE BARYCENTER", "PLUTO BARYCENTER", "SUN", "MERCURY", "VENUS", "MOON", "EARTH", "MARS" } INSTRUMENT_NAME = "N/A" INSTRUMENT_ID = "N/A" SOURCE_PRODUCT_ID = "UNK" NOTE = "SPICE transfer format SPK file." ; pe.bsp LOG FILE ; ; Created 2005-01-02/15:24:45.00. ; ; BEGIN NIOSPK COMMANDS LEAPSECONDS_FILE = /cnav/inputs/naif/naif0007.tls SPK_FILE = pe.bsp INCLUDE_TEXT_FILE = spk_comments_pe.txt INCLUDE_TEXT_FILE = Readme SOURCE_NIO_FILE = /cnav/OD/deliveries/050102_00cTc_orbiter/peph.nio BEGIN_TIME = CAL-ET 2005 JAN 02 15:23:10.182 END_TIME = CAL-ET 2005 JAN 17 11:14:04.183 ; END NIOSPK COMMANDS % template version $Revision: 1.1 $ $Date: 2004/06/10 22:53:01 $ - For OTM-010a based upon OD solution 050102_00cTc_orbiter. This file is invalid after 17-JAN-2005 11:13:00.0 UTC. This file is a planetary ephemeris, only. - FILENAME: 050102AP_PE_05002_05017.BSP PURPOSE OF DELIVERY: OTM-010a (MAS ID O010ae) DELIVERY DATE: 050102 PLANETARY EPHEMERIS USED: from OD delivery SATELLITE/ASTEROID/ROCK EPHEMERIS USED: from OD delivery START EPOCH OF FILE: 2-JAN-2005 15:22:06.0 UTC SCET END EPOCH OF FILE: 17-JAN-2005 11:13:00.0 UTC SCET ------ COMMENTS FROM NAV/OD FOR DELIVERY 050102_00cTc_orbiter -------------------------------------------------------------------------------- DELIVERY NAME: 050102_00cTc BY: John Bordi DATE: January 2, 2005 PURPOSE OF DELIVERY: Final ODM-cleanup OD Delivery ORIGINAL DIRECTORY: /cnav/OD/ops/00cTc/otm010a/epoch_041124/050102 case 9 COMMENTS: Epoch of arc is November 24, 2004 2-way Doppler and Range through 02-JAN-2005 17:17 Optical Data through 27-DEC-2004 18:01 4 WA Probe opnavs are included at 0.25 pixel weight 2 NA Probe opnavs are included at 1.00 pixel weight Using combined planetary_SAT188 covariance with scale factor of 1, State covariance with scale factor of 5 Weights by pass for F2 and SRA Satellites at psf weight Stars at 0.25 pixel Separation uncertainty is 12 mm/s on the probe Tighted stochastics during separation activities to 5.6D-11 and 2*28.D-12 Added nominal value for RCS event during Star ID unsuspend. RCS DV file: estimated small forces until 2004-12-13 12:27:53.000 update on 07-Dec to update events associated with no OTM007 update on 15-Dec to update times associated with OTM008 and values for S06, Dec 17-Jan 16 update on 16-Dec to update prediction for bias/transition to wheels on after separation update on 19-Dec to update times associated with OTM009 RWA bias update on 20-Dec to remove post PTM-cu and ODM-cu RWA biases and adjust the following spin-down DV's update on 24-Dec to update detumble/point to Earth DV after separation update on 26-Dec to update RWA bias after separation with AACS telemtry value update on 27-Dec update times of RWA biases associated with ODM Attitude file used until 17-Jan-2005 and then -Z to Earth, X to north ecliptic Separation masses and orbiter DV updated from Dec 20, 2004 12:18 MAS Run. Decreased detumble uncertainty 5 mm/s Used Troy's updated execution error model scaled by 2 for PTM-cleanup Added 12 mm/s uncertainty for the probe release ---------------------------------------------------------------------------------- \beginlabel MISSION_NAME = "CASSINI" SPACECRAFT_NAME = "CASSINI" DATA_SET_ID = "SPICE_SPK_FILE" KERNEL_TYPE_ID = "SPK" PRODUCT_ID = "050102AP_PE_05002_05017.xsp" PRODUCT_CREATION_TIME = 2005-01-02T15:24:49 PRODUCER_ID = "CASSINI_NAV" MISSION_PHASE_NAME = "TOUR" PRODUCT_VERSION_TYPE = "PREDICT" PLATFORM_OR_MOUNTING_NAME = "N/A" START_TIME = 2005-01-02T15:22:06 STOP_TIME = 2005-01-17T11:13:00 SPACECRAFT_CLOCK_START_COUNT = "N/A" SPACECRAFT_CLOCK_STOP_COUNT = "N/A" TARGET_NAME = { "MERCURY BARYCENTER", "VENUS BARYCENTER", "EARTH BARYCENTER", "MARS BARYCENTER", "JUPITER BARYCENTER", "SATURN BARYCENTER", "URANUS BARYCENTER", "NEPTUNE BARYCENTER", "PLUTO BARYCENTER", "SUN", "MERCURY", "VENUS", "MOON", "EARTH", "MARS" } INSTRUMENT_NAME = "N/A" INSTRUMENT_ID = "N/A" SOURCE_PRODUCT_ID = "UNK" NOTE = "SPICE transfer format SPK file." \endlabel Brief. Version: 2.2.0 (SPICE Toolkit N0055) Summary for: 050102AP_PE_05002_05017.bsp Bodies Start of Interval (ET) End of Interval (ET) ------- ----------------------------- ----------------------------- 1 MERCURY BARYCENTER 2005 JAN 02 15:23:10.183 2005 JAN 17 11:14:04.184 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