MISSION_NAME = "CASSINI" SPACECRAFT_NAME = "CASSINI" DATA_SET_ID = "SPICE_SPK_FILE" KERNEL_TYPE_ID = "SPK" PRODUCT_ID = "100803BP_SK_10215_10232.xsp" PRODUCT_CREATION_TIME = 2010-08-03T11:23:46 PRODUCER_ID = "CASSINI_NAV" MISSION_PHASE_NAME = "TOUR" PRODUCT_VERSION_TYPE = "PREDICT" PLATFORM_OR_MOUNTING_NAME = "N/A" START_TIME = 2010-08-03T11:20:16 STOP_TIME = 2010-08-20T07:58:55 SPACECRAFT_CLOCK_START_COUNT = "N/A" SPACECRAFT_CLOCK_STOP_COUNT = "N/A" TARGET_NAME = "CASSINI" INSTRUMENT_NAME = "N/A" INSTRUMENT_ID = "N/A" SOURCE_PRODUCT_ID = "SEE COMMENTS" NOTE = "SPICE transfer format SPK file." ; bp_sk.bsp LOG FILE ; ; Created 2010-08-03/11:23:41.00. ; ; BEGIN NIOSPK COMMANDS LEAPSECONDS_FILE = /cnav/inputs/naif/latest.tls SPK_FILE = bp_sk.bsp INCLUDE_TEXT_FILE = spk_comments_bp_sk.txt INCLUDE_TEXT_FILE = Readme SOURCE_NIO_FILE = /cnav/OD/deliveries/100803_135E11/p.nio BODIES = -82 BEGIN_TIME = CAL-ET 2010 AUG 03 11:21:20.898 END_TIME = CAL-ET 2010 AUG 20 08:00:00.000 ; END NIOSPK COMMANDS % template version $Revision: 1.13 $ $Date: 2006/08/18 20:07:09 $ - For OTM-259 based upon OD solution 100803_135E11. This file is invalid after 20-AUG-2010 08:00:00.0000 ET or execution of subsequent maneuvers. This file does not include OTM-259 or its effects. Maneuvers prior to OTM-259 are included. This file is a spacecraft ephemeris only. This file should only be used in case OTM-259 is NOT implemented. - FILENAME: 100803BP_SK_10215_10232.BSP PURPOSE OF DELIVERY: OTM-259 (MAS ID O259_d) DELIVERY DATE: 100803 PLANETARY EPHEMERIS USED: from OD delivery SATELLITE/ASTEROID/ROCK EPHEMERIS USED: from OD delivery START EPOCH OF FILE: 3-AUG-2010 11:21:20.9 ET SCET END EPOCH OF FILE: 20-AUG-2010 08:00:00.0000 ET SCET ------ COMMENTS FROM NAV/MVR FOR OTM-259 O259_d By: Cassini-Huygens Navigation Team Profile file: MPF_O259_d_100803_135E11 Maneuver Start: 10-AUG-2010 22:35:00.000 UTC SCET ------ COMMENTS FROM NAV/OD FOR DELIVERY 100803_135E11 ----------------------------------------------------------------------------- DELIVERY NAME: 100803_135E11 BY: Kevin Criddle DATE: August 03, 2010 PURPOSE OF DELIVERY: Preliminary OD Delivery for OTM259 ORIGINAL DIRECTORY: /cnav/OD/ops/135E11/epoch_100627/otm259/100803 case 7 COMMENTS: Epoch of arc is 27-JUN-2010 12:00:00.0 ET Spacecraft a priori state and covariance from previous arc Spacecraft State covariance with scale factor of 5 Satellite/planet Covariance based on sat335 2-way Doppler and Range through 03-AUG-2010 17:00 Optical Data through 02-JUN-2010 23:35 (none in this arc) Weights by pass for F2 and SRA SMALL FORCES: SMFDV001 30-JUN-2010 07:01:19.3 RWA spindown before OTM-255 SMFDV002 30-JUN-2010 08:29:42.6 RWA spinup after OTM-255 SMFDV003 30-JUN-2010 09:17:10.7 Redundant post-OTM background sequence RWA bias SMFDV004 02-JUL-2010 10:31:15.5 RWA bias (using y-thrusters) SMFDV005 03-JUL-2010 23:40:21.5 RWA bias before OTM-256 SMFDV006 04-JUL-2010 02:17:03.3 RWA bias after OTM-256 SMFDV007 04-JUL-2010 19:05:11.8 RWA bias (standard) SMFDV008 05-JUL-2010 23:58:58.6 RWA bias (using y-thrusters) SMFDV010 07-JUL-2010 00:57:44.4 RWA spinup after T71-flyby SMFDV011 10-JUL-2010 06:18:15.8 RWA spindown before OTM-257 SMFDV012 10-JUL-2010 07:39:04.2 RWA spinup after OTM-257 SMFDV013 10-JUL-2010 08:31:17.7 Redundant post-OTM background sequence RWA bias SMFDV014 18-JUL-2010 05:57:50.7 RWA spindown before OTM-258 SMFDV015 18-JUL-2010 07:30:28.7 RWA spinup after OTM-258 SMFDV016 18-JUL-2010 08:13:05.7 Redundant post-OTM background sequence RWA bias SMFDV017 23-JUL-2010 16:44:45.6 RWA bias (using y-thrusters) SMFDV018 26-JUL-2010 00:26:08.5 RWA bias (using y-thrusters) SMFDV019 30-JUL-2010 08:35:07.5 RWA bias (using y-thrusters) SMFDV020 01-AUG-2010 14:42:25.3 RWA bias MANEUVERS OTM-255, 30-JUN-2010 6.25 m/s ME, telemetry-based pointing model OTM-256, 04-JUL-2010 22.8 mm/s RCS,telemetry-based pointing model OTM-257, 10-JUL-2010 0.84 m/s ME, telemetry-based pointing model OTM-258, 18-JUL-2010 6.77 m/s ME, telemetry-based pointing model ------------------------------------------------------------------------------- \beginlabel MISSION_NAME = "CASSINI" SPACECRAFT_NAME = "CASSINI" DATA_SET_ID = "SPICE_SPK_FILE" KERNEL_TYPE_ID = "SPK" PRODUCT_ID = "100803BP_SK_10215_10232.xsp" PRODUCT_CREATION_TIME = 2010-08-03T11:23:46 PRODUCER_ID = "CASSINI_NAV" MISSION_PHASE_NAME = "TOUR" PRODUCT_VERSION_TYPE = "PREDICT" PLATFORM_OR_MOUNTING_NAME = "N/A" START_TIME = 2010-08-03T11:20:16 STOP_TIME = 2010-08-20T07:58:55 SPACECRAFT_CLOCK_START_COUNT = "N/A" SPACECRAFT_CLOCK_STOP_COUNT = "N/A" TARGET_NAME = "CASSINI" 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: 100803BP_SK_10215_10232.bsp Bodies Start of Interval (ET) End of Interval (ET) ------- ----------------------------- ----------------------------- -82 CASSINI 2010 AUG 03 11:21:20.899 2010 AUG 20 08:00:00.000