MISSION_NAME = "CASSINI" SPACECRAFT_NAME = "CASSINI" DATA_SET_ID = "SPICE_SPK_FILE" KERNEL_TYPE_ID = "SPK" PRODUCT_ID = "071114AP_PE_07318_07328.xsp" PRODUCT_CREATION_TIME = 2007-11-14T11:38:39 PRODUCER_ID = "CASSINI_NAV" MISSION_PHASE_NAME = "TOUR" PRODUCT_VERSION_TYPE = "PREDICT" PLATFORM_OR_MOUNTING_NAME = "N/A" START_TIME = 2007-11-13T02:54:55 STOP_TIME = 2007-11-24T11:58:55 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 = "SEE COMMENTS" NOTE = "SPICE transfer format SPK file." ; pe_nowrap.bsp LOG FILE ; ; Created 2007-11-14/11:38:17.00. ; ; BEGIN NIOSPK COMMANDS LEAPSECONDS_FILE = /cnav/inputs/naif/latest.tls SPK_FILE = pe_nowrap.bsp INCLUDE_TEXT_FILE = spk_comments_pe.txt INCLUDE_TEXT_FILE = Readme SOURCE_NIO_FILE = /cnav/OD/deliveries/071114_052T37/peph.nio BEGIN_TIME = CAL-ET 2007 NOV 13 02:56:00.000 END_TIME = CAL-ET 2007 NOV 24 12:00:00.000 ; END NIOSPK COMMANDS % template version $Revision: 1.4 $ $Date: 2006/08/18 20:07:24 $ - For OTM-133 based upon OD solution 071114_052T37. This file is invalid after 24-NOV-2007 12:00:00.00 ET. This file is a planetary ephemeris, only. - FILENAME: 071114AP_PE_07318_07328.BSP PURPOSE OF DELIVERY: OTM-133 (MAS ID O133_g) DELIVERY DATE: 071114 PLANETARY EPHEMERIS USED: from OD delivery SATELLITE/ASTEROID/ROCK EPHEMERIS USED: from OD delivery START EPOCH OF FILE: 13-NOV-2007 02:56:00.0 ET SCET END EPOCH OF FILE: 24-NOV-2007 12:00:00.00 ET SCET ------ COMMENTS FROM NAV/OD FOR DELIVERY 071114_052T37 -------------------------------------------------------------------------------- DELIVERY NAME: 071114_052T37 BY: Paul F. Thompson DATE: November 14, 2007 PURPOSE OF DELIVERY: Final OTM133 OD Delivery ORIGINAL DIRECTORY: /cnav/OD/ops/052T37/epoch_071014/otm133/071114 case 4 COMMENTS: Epoch of arc is 14-OCT-2007 12:00:00.000000000 Spacecraft a priori state and covariance from sat264 delivery Spacecraft State covariance with scale factor of 5 Satellite/planet Covariance sat264 2-way Doppler and Range through 14-NOV-2007 16:00 Optical Data through 09-NOV-2007 19:20 Weights by pass for F2 and SRA SMALL FORCES: SMFDV001 18-OCT-2007 16:42:11.0 RWA bias SMFDV002 23-OCT-2007 06:03:16.4 RWA bias SMFDV003 26-OCT-2007 06:09:51.3 Friction Test spinup SMFDV004 26-OCT-2007 07:05:37.6 Friction Test coastdown SMFDV005 26-OCT-2007 08:15:07.4 Friction Test spinup SMFDV006 26-OCT-2007 08:48:09.6 Friction Test coastdown SMFDV007 26-OCT-2007 09:54:38.3 Friction Test bias SMFDV008 28-OCT-2007 14:24:10.6 BU Friction Test spinup SMFDV009 28-OCT-2007 15:21:51.1 BU Friction Test coastdown SMFDV010 28-OCT-2007 16:01:14.6 BU Friction Test spinup SMFDV011 28-OCT-2007 16:44:36.1 BU Friction Test coastdown SMFDV012 28-OCT-2007 17:35:34.1 BU Friction Test bias SMFDV013 01-NOV-2007 15:07:24.3 OTM132 spindown SMFDV014 01-NOV-2007 16:26:40.4 OTM132 bias SMFDV015 09-NOV-2007 15:06:42.1 RWA bias MANEUVERS OTM132: estimated ME burn using telem values and sigmas for pointing NOTES Backup friction test apriori values from FSDS predicts replaced with values estimated from OD due to the fact that predicts were off by well over 2.5 mm/s. Apriori sigmas for pointing (RA,DEC) of both the prime and backup friction tests were increased from 1 deg to 5 deg. ------------------------------------------------------------------------------------- \beginlabel MISSION_NAME = "CASSINI" SPACECRAFT_NAME = "CASSINI" DATA_SET_ID = "SPICE_SPK_FILE" KERNEL_TYPE_ID = "SPK" PRODUCT_ID = "071114AP_PE_07318_07328.xsp" PRODUCT_CREATION_TIME = 2007-11-14T11:38:39 PRODUCER_ID = "CASSINI_NAV" MISSION_PHASE_NAME = "TOUR" PRODUCT_VERSION_TYPE = "PREDICT" PLATFORM_OR_MOUNTING_NAME = "N/A" START_TIME = 2007-11-13T02:54:55 STOP_TIME = 2007-11-24T11:58:55 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 = "SEE COMMENTS" NOTE = "SPICE transfer format SPK file." \endlabel Brief. Version: 2.2.0 (SPICE Toolkit N0058) Summary for: 071114AP_PE_07318_07328.bsp Bodies Start of Interval (ET) End of Interval (ET) ------- ----------------------------- ----------------------------- 1 MERCURY BARYCENTER 2007 NOV 13 02:56:00.000 2007 NOV 24 12:00:00.000 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