PDS_VERSION_ID = PDS3 LABEL_REVISION_NOTE = " 2009-02-23 NAIF:Semenov original; 2009-09-21 NAIF:Semenov fixed a few typos; 2011-06-23 NAIF:Semenov updated for DIXI data; 2011-09-07 NAIF:Semenov updated for version 2 high-rate CK, fixed typos; 2021-04-12 NAIF:Costa updated CITATION_DESC with DOI; " RECORD_TYPE = STREAM OBJECT = DATA_SET DATA_SET_ID = "DIF-C/E/X-SPICE-6-V1.0" OBJECT = DATA_SET_INFORMATION DATA_SET_NAME = "EPOXI SPICE KERNELS V1.0" DATA_SET_COLLECTION_MEMBER_FLG = "N" DATA_SET_TERSE_DESC = " Navigation and ancillary data in the form of SPICE System kernel files for the EPOXI mission. " ABSTRACT_DESC = " This data set includes the complete set of EPOXI SPICE data files (``kernel files''), which can be accessed using SPICE software. The SPICE data contains geometric and other ancillary information needed to recover the full value of the science instrument data. In particular SPICE kernels provide spacecraft and planetary ephemerides, instrument mounting alignments, spacecraft orientation, spacecraft sequences of events, and data needed for relevant time conversions. " CITATION_DESC = " Semenov, B.V., and C.H. Acton, EPOXI SPICE KERNELS V1.0, DIF-C/E/X-SPICE-6-V1.0, NASA Planetary Data System, 2009. https://doi.org/10.17189/1520118 " START_TIME = 2005-08-23T17:19:48 STOP_TIME = 2011-03-01T00:59:44 DATA_SET_RELEASE_DATE = 2009-03-01 PRODUCER_FULL_NAME = "BORIS V. SEMENOV" DATA_OBJECT_TYPE = "SPICE KERNEL" DETAILED_CATALOG_FLAG = "Y" DATA_SET_DESC = " Data Set Overview ================= This data set includes the complete set of EPOXI SPICE data files (``kernel files''), which can be accessed using SPICE software. The SPICE data contains geometric and other ancillary information needed to recover the full value of the science instrument data. In particular SPICE kernels provide spacecraft and planetary ephemerides, instrument mounting alignments, spacecraft orientation, spacecraft sequences of events, and data needed for relevant time conversions. Data Types (SPICE kernel types) =============================== SPK kernels contain ephemerides for spacecraft, planets, satellites, comets and asteroids as well as for moving or fixed spacecraft and instrument structures. They provide position and velocity, given in a Cartesian reference frame. SPK files are located under the ``data/spk'' directory of this data set. PCK kernels contain certain physical, dynamical and cartographic constants for target bodies, such as size and shape specifications, and the orientation of the spin axis and prime meridian. PCK files are located under the ``data/pck'' directory of this data set. IK kernels (Instrument description kernels) give descriptive and operational data peculiar to a particular scientific instrument, such as internal timing relative to the spacecraft clock and field-of-view model parameters. IK files are located under the ``data/ik'' directory of this data set. CK kernels describe pointing, containing a transformation traditionally called the C-matrix which is used to determine time-tagged pointing (orientation) angles for a spacecraft structure upon which science instruments are mounted. CK files are located under the ``data/ck'' directory of this data set. EK (Events) kernels are derived from the integrated sequence of events used to produce actual spacecraft commands. EK files are located under the ``data/ek'' directory of this data set. LSK (Leapseconds) kernels contain the leapseconds and the values of other constants required to perform a transformation between Universal Time Coordinated (UTC) and Ephemeris time (ET). LSK files are located under the ``data/lsk'' directory of this data set. SCLK (Spacecraft Clock) kernels contain on-board clock calibration data required to perform a mapping between Ephemeris time (ET) and spacecraft on-board time (SCLK.) SCLK files are located under the ``data/sclk'' directory of this data set. FK (Frame Definitions) kernels contain information required to define reference frames, sources of frame orientation data and inter-connections between these frames and other frames supported within the SPICE system. This includes mounting alignment information for each instrument. FK files are located under the ``data/fk'' directory of this data set. Kernel File Details =================== A brief overview of the different types of EPOXI kernels included in this data set is provided in the CONFIDENCE_LEVEL_NOTE section of this file while details specific to individual files are found in the ``*info.txt'' files in the corresponding data directory. The most detailed description of the data in each file is provided in metadata included inside the file -- in the description area of text kernels or in the comment area of binary kernels. Software ======== The SPICE Toolkit contains software modules needed to read SPICE kernel files. SPICELIB software is highly documented via internal headers. Additional documentation is available in separate ASCII text files called Required Reading files. For example, the S- and P- Kernel (SPK) Required Reading File, named SPK.REQ, describes use of the SPK kernel file readers and contains sample programs. The latest SPICE Toolkit for a variety of computer platforms such as PC, Mac, SUN, etc. is available at the NAIF Node of PDS electronically (via anonymous FTP and WWW servers). Refer to information in ``software/softinfo.txt'' for details regarding obtaining this software. Each version of the Toolkit is also archived at the NASA National Space Science Data Center. Loading Kernel Files into a SPICE-based Application =================================================== The easiest way to make data from a collection of SPICE kernels available to a SPICE-based application is to list these kernels in a meta-kernel and load it into the program using the high level SPICE data loader routine FURNSH. This data set provides such meta-kernel(s) under the ``extras/mk'' directory. For more information about the EPOXI meta-kernel(s), see the file ``extras/mk/mkinfo.txt''. " CONFIDENCE_LEVEL_NOTE = " This data set contains SPICE kernel files created during mission operations and after mission data reconstruction and analysis. Some general information about this collection follows here, but the prospective user is also referred to extensive descriptions about each file that are stored inside each kernel file. These metadata provide detailed information regarding the information source from which the data were derived, the type of processing applied to the source data, applicability of the data, etc. Metadata are located in the ``comment area'' for binary kernel types (SPK, CK, ESQ), accessible using either the COMMNT or SPACIT utility program found in the NAIF Toolkit. Metadata are located after ``\begintext'' markers within the text kernel types (PCK, IK, FK, LSK, SCLK), accessible by using any available text file display tool such as a word processor, text editor, or the UNIX ``more'' or ``cat'' commands. In some cases data accuracy information does not exist because it could not be estimated even after mission completion. Where there are questions about data accuracy or ``confidence'' not addressed herein the reader is invited to examine subsequent SPICE archive releases associated with this data set (if such exist), or to contact the NAIF node of the Planetary Data System for possible further information. SPK Files ========= The SP-Kernel files included in this data set provide reconstructed trajectory of the Deep Impact Flyby (DIF) spacecraft and ephemeris data for the mission target comet Hartley 2, Solar System planets, and the Sun. Additional information about SPK files provided in this data set is available in the file ``data/spk/spkinfo.txt''. CK Files ======== C-kernel files included in this data set provide the orientation of the DIF spacecraft bus and the DIF high gain antenna (HGA). Some of these CK files were produced from engineering telemetry downlinked from the spacecraft; others, containing predicted data, were produced by attitude simulation tools based on the planned attitude profiles. As is often the case with spacecraft engineering telemetry-based measurements, considerable uncertainty exists as to the accuracy of such measurements, and, data quality (accuracy and completeness) can vary significantly. DIF Spacecraft Bus CK files --------------------------- Three kinds of the DIF spacecraft bus orientation CK files are included in this data set. The first kind are reconstructed attitude kernels based on the low rate telemetry (1/8 Hz). The coverage provided by these files is full of gaps, which due to the attitude data downlink strategy frequently happen at the times of transitions between different attitude modes, making interpolation over these gaps produce grossly incorrect attitude. For this reason the interpolation intervals in these reconstructed files should not be altered using CKSPANIT or a similar tool. The second kind is the reconstructed attitude kernel based on the high rate telemetry (up to 5 Hz) providing coverage only for about 8 hour period around closest approach to Hartley 2. The version 1 of this CK had internal time tags truncated by up to 2 milliseconds, introducing attitude errors of almost 30 microradians during the fastest spacecraft turn rates in the ~200 second interval around the closest approach to Hartley 2 (at other times attitude errors due to this truncation were negligible). This problem was fixed in the version 2 of this CK. The accuracy of the DIF spacecraft bus orientation determined on-board and stored in the low- and high- CK files varied significantly, from 50 micro-radians (~5 MRI pixels) at the times when the attitude was determined based on the star tracker measurements to a few hundreds of micro-radians (tens of MRI pixels) for the periods when the attitude was determined by propagating ACS gyro data without any star tracker updates for extended periods of time. The third kind are predicted kernels providing nominal attitude for the whole or a part of the mission or just for the periods of target star observations during the EPOCh part of the mission. The predicted files were generated using prediCkt tool and are included in the data set with the sole purpose of providing some attitude for the periods when the reconstructed files have gaps. Although a comparison of reconstructed and predicted CK files for the periods when both provided coverage showed that in many cases the predicted CK data matched the actual attitude to a fraction of degree, the accuracy of the predicted CK files in general is suspect because of the idealistic attitude modeling rules, incorrect timing of attitude mode transitions, and lack of modeling of some spacecraft activities altogether. Any users of the predicted CKs are encouraged to compare them against the reconstructed CKs during the period(s) of interest using the FRMDIFF tool provided in the SPICE toolkit to assess the differences. All three types of files need to be loaded at the same time to provide the most complete coverage with the predicted CKs loaded first so that data from them is accessed last (lowest priority), the low rate CKs with corrected times tags (v2) loaded second (medium priority), and the high rate CK for the encounter loaded last (highest priority). DIF HGA CK Files ---------------- Two kinds of the DIF HGA orientation CK files are included in this data set. The first kind is based on the measured HGA gimbal angles provided in telemetry (``V-channels'') while the second kind is based on the commanded HGA gimbal angles provided in telemetry (``B-channels''). These files should be loaded together to provide the most complete coverage with the file based on measured angles loaded last (to be accessed first.) Even when loaded together, the combined coverage provided by the files is full of gaps, which can be alleviated by modifying the interpolation interval information by using the CKSPANIT program. Additional information about CK files provided in this data set is available in the file ``data/ck/ckinfo.txt''. PCK Files ========= PCK files provide size, shape and orientation data for ``target'' bodies such as planets, satellites, comets and asteroids. A description of these data items and reference to their source is provided inside the PCK file, which is a simple text file that can be viewed using any word processor, text editor or text display utility. This data set contains generic PCK file based on the official IAU/IAG/COSPAR values accepted in 2000 and PCK file for EPOXI mission target -- Hartley 2 -- providing constants determined after the encounter. The PCK file for Hartley 2 contains both rotation and shape/size data derived by the EPOXI science team during post encounter data analysis. Additional information about PCK files provided in this data set is available in the file ``data/pck/pckinfo.txt''. FK Files ======== Frames kernel files provide specifications for how one reference frame is defined relative to another frame. The DI FK provided in this data set contains a complete set of frame definitions for the both spacecraft, their structures such as antennas, and all of their science instruments. Comments in the FK file provide the frame definitions, a description of the frame relationships, the source of and accuracy of the mounting alignment information, etc. The instrument frame definitions provided in the file incorporate the latest mounting alignment data available at the end of the mission. Additional information about FK files provided in this data set is available in the file ``data/fk/fkinfo.txt''. IK Files ======== Instrument kernel files provide specifications for the optical and physical instrument parameters and -- where applicable -- field-of-view size, shape and orientation for the named instrument. Metadata describing these estimates are provided in each IK file included in this archive. While a majority of the of parameters included in the IK files archived in this data set are based on the nominal instrument data, the files incorporate the latest version of optical distortion model derived by the DI optical navigation team. Additional information about IK files provided in this data set is available in the file ``data/ik/ikinfo.txt''. SCLK Files ========== Spacecraft Clock kernel files provide a tabulation of data needed to convert time measurements between ephemeris time (ET) and spacecraft clock time (SCLK). A SPICE SCLK file is made from a similar file -- SCLK/SCET or SCLKvSCET file -- produced by another mission entity. Each newly made SCLK file fully replaces the previous SCLK file. This data set includes SCLK kernels providing the correlations for the DIF spacecraft primary (SCU-A) and secondary (SCU-B) on-board clocks. Two SCLK kernels -- the ``official'' version and ``science'' version -- are available for the DIF primary clock while only one SCLK kernel -- ``official'' version -- is available for the DIF secondary clock. The main difference between the ``official'' version of the primary clock SCLK kernel and the ``science'' version is that the ``official'' version is based on the latest time correlation that were used by the project during mission operations while the ``science'' version contain updated correlation that were used to process science data for archiving in PDS. The correlation update for the DIF primary clock SCLK kernel was done to eliminate ``artificial'' data points introduced by the tool-set that created source SCLKvSCET file and to adjust clock rates in order to connect actual data points in a continuous fashion. Such ``artificial'' data points were eliminated only during two periods -- 2009-01-06 to 2010-10-27 and 2010-11-17 to 2011-03-01 -- because the ``official'' correlation prior to 2009-01-06 and around Hartley 2 encounter did not need such adjustments. Unfortunately, the absolute accuracy of both ``official'' and ``science'' correlations for all periods EXCEPT for the period around Hartley 2 encounter (2010-10-27 to 2010-11-17) is no better than 0.5 seconds due to poor quality of the source clock correlations data. For the encounter period the correlation has much better accuracy, down to .01 seconds for evaluating SCLK -> UTC around closest approach, thanks to efforts by Steve Wissler and Amy Walsh of EPOXI Spacecraft Team in correcting and re-fitting the source correlation data Note that the clock format defined by both ``official'' and ``science'' SCLK kernels (seconds with fractional seconds given as a count of 1/256 second ticks) does not match the format of on-board time tags in mission telemetry (seconds with fractional seconds given as top 8 or 16 or full 20 bits of a count of micro-seconds). For details on this discrepancy and the algorithm to fix it see ``sclk140.txt'' provided in Deep Impact and EPOXI documentation set (DI-C-HRII/HRIV/MRI/ITS-6-DOC-SET-V3.0). While all science images sent to the ground contained SCLK time in the headers (spacecraft primary, SCU-A, SCLK for DIF), optical- and auto-navigation image headers contain a different time. This time was a so called on-board Ephemeris Time (ET) that optical/auto navigation on-board software used internally to perform autonomous trajectory and attitude solutions. This on-board ET was computed from on-board clock by adding a constant delta to it to make it synchronous with the actual ET to the extent possible. Since the on-board clock was drifting throughout the mission, the delta had to be changed many times. The table below shows the delta, in seconds, that must be subtracted from the on-board ET to get corresponding SCLK (spacecraft primary, SCU-A, SCLK for DIF) and the time when a particular delta had been uplinked and took effect in the on-board software (shown as UTC): Applicability Start UTC Delta ----------------------- -------- 2007-351T17:35:02.1287 512.325 2007-363T17:25:04.4477 525.293 2008-078T16:12:19.5120 665.717 2008-105T23:24:20.9104 732.653 2008-137T03:57:41.1835 821.037 2008-142T10:13:15.6053 857.544 2008-151T19:54:10.8499 875.314 2008-165T17:57:03.9399 897.396 2008-184T11:28:57.2223 806.231 2008-212T17:28:54.5972 839.715 2008-240T04:28:57.5992 864.011 2008-268T02:58:58.9329 890.432 2008-319T23:59:00.3904 943.327 2008-349T23:59:08.6112 969.590 2009-005T21:59:15.8754 989.965 2009-046T00:14:05.8648 1056.877 2009-074T00:14:07.1411 1095.119 2009-083T22:13:28.6435 1121.229 2009-105T00:13:59.7459 1146.244 2009-135T00:13:59.6404 1187.763 2009-147T08:03:22.1973 1213.564 2009-153T06:34:59.1203 1223.314 2009-166T00:13:58.7132 1230.997 2009-182T11:59:00.0174 1252.004 2009-196T00:13:59.7825 1270.692 2009-227T00:14:00.0946 1311.956 2009-258T00:14:00.1187 1354.722 2009-268T15:30:09.3380 1371.659 2009-275T18:51:55.1384 1382.729 2009-288T00:14:01.1509 1396.132 2009-316T17:19:33.1640 1449.351 2009-319T00:14:05.5821 1435.769 2009-337T11:32:02.5265 1471.203 2009-344T19:02:28.8364 1481.542 2009-349T00:14:02.2259 1483.738 2009-351T15:28:11.1679 1490.387 2009-358T21:14:01.2625 1499.945 2010-001T02:14:01.7135 1510.532 2010-015T00:14:02.6994 1530.969 2010-046T00:13:58.9541 1581.193 2010-071T17:35:08.3947 1623.057 2010-074T00:13:58.9368 1622.033 2010-105T00:13:58.3922 1666.541 2010-135T00:13:59.2603 1708.935 2010-166T00:13:59.4915 1750.700 2010-183T20:58:59.3697 1775.852 2010-190T20:39:27.8465 1789.371 2010-196T00:13:59.4687 1792.938 2010-227T00:14:02.0552 1835.460 2010-246T18:50:23.1339 1866.382 2010-258T00:13:53.1890 1878.792 2010-272T20:47:43.1103 1906.565 2010-288T10:54:55.5247 1927.342 2010-289T08:49:17.9432 1924.467 2010-300T19:05:35.6008 1939.803 2010-307T19:16:24.8070 1949.819 2010-319T00:13:56.3420 1973.249 2010-349T00:14:00.1550 1999.840 2011-015T00:13:52.2455 2037.864 2011-046T00:13:44.2797 2076.248 2011-074T00:13:54.5237 2087.404 2011-105T00:14:01.1949 2105.201 2011-135T00:14:10.3797 2127.709 2011-166T00:13:42.7977 2176.681 Additional information about SCLK files provided in this data set is available in the file ``data/sclk/sclkinfo.txt''. LSK Files ========= Leapseconds kernel files provide a tabulation of ``leapseconds'' and some other terms used in converting time measurements between ephemeris time (ET) and Universal Time (UTC). ``Spacecraft Event Time'' (SCET) is the commonly used name for UTC events measured at the spacecraft. Metadata describing how the LSK data are obtained or computed is contained inside the LSK text file. The time conversion provided by SPICE LSK files is accurate to approximately 0.000030 seconds. Additional information about LSK files provided in this data set is available in the file ``data/lsk/lskinfo.txt''. EK Files ======== No Events kernel (EK) files are included in this archive. Kernel Files Not Included In This Data Set =========================================== A number of kernel files used to process image data archived in PDS and mentioned in the image labels were not included in this data set because they either were superseded by the files provided in this archive, or were known to contain incorrect or out-of-date information, or could be easily re-created from the data provided in this archive using utility program(s) available from NAIF. Among such files are: - regular OPS SPK files: spk_od218_full.bsp spk_od219_full.bsp spk_od221_full.bsp spk_od222_full.bsp spk_mars_drm232.bsp were superseded by the SPK files ``dif_epoch_nav_v1.bsp'' and ``dif_dixi_nav_v1.bsp'' included in this data set. - Jovian system SPK file jup164_20year.bsp is not included because no observations of Jupiter or its satellites were made during the mission. - SPK file containing an earlier version of Hartley 2 ephemeris hartley_2_2005_2020.bsp was superseded by the SPK file ``dif_dixi_nav_v1.bsp'' included in this data set. - predicted CK files: dif_epoxi_predict_v20081206.bc dif_pred_earthobs4_1.bc were superseded by the predicted CK files ``dif_sc_071103_090127_p.bc'' and ``dif_sc_071103_090127_p_to.bc'' included in this data set. - star position SPK and PCK files: starnames_2008253_074135.tpc starnames_2009338_165219.tpc stars_2008253_074135.bsp stars_2010078_071625.bsp were used in the Science Data Center image processing pipeline to provide access via SPICE interfaces to positions of the mission target stars. While these kernels successfully served their purpose, they were not fully compliant with official NAIF practices. For this reason they were not included into this data set. On the other hand, recognizing the importance of this data, it was decided to include the star positions stored in these files and the NAIF names and ID codes assigned to these stars into this data set's documentation for the reference. The table below provides these positions. Each line contains J2000 RA (hours, minutes, seconds), J2000 DEC (degrees, arcminutes, arcseconds) and name. 10,24,23.71,-74,1,53.8,PRETEND I CAR HD 90589 0,25,45.07,-77,15,15.3,BET HYI HD 2151 10,2,42,-60,7,0,NGC3114 6,23,57.11,-52,41,44.4,CANOPUS HD 45348 1,37,42.85,-57,14,12.3,ACHERNAR HD 10144 21,7,6,42,14,0,NGC7027 19,41,48.95,50,31,30.2,16 CYG A HD 186408 7,33,27.32,-50,35,3.3,HD 60753 18,36,56.34,38,47,1.3,VEGA HD 172167 0,24,5.22,-72,4,57.9,47 TUC NGC104 6,45,08.92,-16,42,58.0,SIRIUS HD 48915 9,11,16.72,-62,19,1.1,I CAR HD 79447 11,5,33,-58,43,48,NGC3532 18,51,6,-6,16,0,M11 10,36,16.079,-58,16,38.20,HD 92044 8,40,36,-53,2,0,OMI VEL CLUSTER IC2391 11,42,11.5968,26,42,16.812,GJ436 22,57,46.8,38,40,27.84,HAT-P-1 16,20,36,41,2,52.8,HAT-P-2 13,44,22.56,48,1,44.4,HAT-P-3 15,19,57.92712,36,13,46.7904,HAT-P-4 19,4,9.84,36,37,58.8,TRES-1 19,7,14.0304,49,18,59.2992,TRES-2 17,52,7.032,37,32,46.1004,TRES-3 17,53,12.96,37,12,43.2,TRES-4 0,20,40.08,31,59,24,WASP-1 20,30,54.24,6,25,48,WASP-2 16,2,11.76,28,10,12,XO-1 7,48,6.4704,50,13,32.988,XO-2 4,21,53.5104,57,49,0.5988,XO-3 9,22,39.7267,50,36,13.927,HD 80607 21,50,54.7530,25,19,07.495,TYC 2206-1748-1 18,34,31.6249,35,39,41.546,WASP-3 19,28,59.3616,47,58,10.264,HAT-P-7 17,48,1.95,-35,00,19.48,MOA-2009-BLG-266 The following NAIF name/ID mappings were assigned to these stars: NAIF_BODY_NAME += ( 'PRETEND I CAR HD 90589' ) NAIF_BODY_CODE += ( 9999000 ) NAIF_BODY_NAME += ( 'BET HYI HD 2151' ) NAIF_BODY_CODE += ( 9999001 ) NAIF_BODY_NAME += ( 'NGC3114' ) NAIF_BODY_CODE += ( 9999002 ) NAIF_BODY_NAME += ( 'CANOPUS HD 45348' ) NAIF_BODY_CODE += ( 9999003 ) NAIF_BODY_NAME += ( 'ACHERNAR HD 10144' ) NAIF_BODY_CODE += ( 9999004 ) NAIF_BODY_NAME += ( 'NGC7027' ) NAIF_BODY_CODE += ( 9999005 ) NAIF_BODY_NAME += ( '16 CYG A HD 186408' ) NAIF_BODY_CODE += ( 9999006 ) NAIF_BODY_NAME += ( 'HD 60753' ) NAIF_BODY_CODE += ( 9999007 ) NAIF_BODY_NAME += ( 'VEGA HD 172167' ) NAIF_BODY_CODE += ( 9999008 ) NAIF_BODY_NAME += ( '47 TUC NGC104' ) NAIF_BODY_CODE += ( 9999009 ) NAIF_BODY_NAME += ( 'SIRIUS HD 48915' ) NAIF_BODY_CODE += ( 9999010 ) NAIF_BODY_NAME += ( 'I CAR HD 79447' ) NAIF_BODY_CODE += ( 9999011 ) NAIF_BODY_NAME += ( 'NGC3532' ) NAIF_BODY_CODE += ( 9999012 ) NAIF_BODY_NAME += ( 'M11' ) NAIF_BODY_CODE += ( 9999013 ) NAIF_BODY_NAME += ( 'HD 92044' ) NAIF_BODY_CODE += ( 9999014 ) NAIF_BODY_NAME += ( 'OMI VEL CLUSTER IC2391' ) NAIF_BODY_CODE += ( 9999015 ) NAIF_BODY_NAME += ( 'GJ436' ) NAIF_BODY_CODE += ( 9999016 ) NAIF_BODY_NAME += ( 'HAT-P-1' ) NAIF_BODY_CODE += ( 9999017 ) NAIF_BODY_NAME += ( 'HAT-P-2' ) NAIF_BODY_CODE += ( 9999018 ) NAIF_BODY_NAME += ( 'HAT-P-3' ) NAIF_BODY_CODE += ( 9999019 ) NAIF_BODY_NAME += ( 'HAT-P-4' ) NAIF_BODY_CODE += ( 9999020 ) NAIF_BODY_NAME += ( 'TRES-1' ) NAIF_BODY_CODE += ( 9999021 ) NAIF_BODY_NAME += ( 'TRES-2' ) NAIF_BODY_CODE += ( 9999022 ) NAIF_BODY_NAME += ( 'TRES-3' ) NAIF_BODY_CODE += ( 9999023 ) NAIF_BODY_NAME += ( 'TRES-4' ) NAIF_BODY_CODE += ( 9999024 ) NAIF_BODY_NAME += ( 'WASP-1' ) NAIF_BODY_CODE += ( 9999025 ) NAIF_BODY_NAME += ( 'WASP-2' ) NAIF_BODY_CODE += ( 9999026 ) NAIF_BODY_NAME += ( 'XO-1' ) NAIF_BODY_CODE += ( 9999027 ) NAIF_BODY_NAME += ( 'XO-2' ) NAIF_BODY_CODE += ( 9999028 ) NAIF_BODY_NAME += ( 'XO-3' ) NAIF_BODY_CODE += ( 9999029 ) NAIF_BODY_NAME += ( 'HD 80607' ) NAIF_BODY_CODE += ( 9999030 ) NAIF_BODY_NAME += ( 'TYC 2206-1748-1' ) NAIF_BODY_CODE += ( 9999031 ) NAIF_BODY_NAME += ( 'WASP-3' ) NAIF_BODY_CODE += ( 9999032 ) NAIF_BODY_NAME += ( 'HAT-P-7' ) NAIF_BODY_CODE += ( 9999033 ) NAIF_BODY_NAME += ( 'MOA-2009-BLG-266' ) NAIF_BODY_CODE += ( 9999034 ) - text kernel providing times of encounter for the SDC pipeline impacttoi_0007h2.tpc This text kernel had the following contents: Deep Impact/EPOXI at Hartley 2 Local times of DI TCA Hartley 2 as a leapsecond-corrected UTC EOB_TOI: local time that photons from Hartley 2 reach the Earth DIF_TOI: local time that photons from Hartley 2 reach the Deep Impact Flyby S/C DII_TOI: local time that the Deep Impact Impactor S/C hits Tempel 1 \begindata EOB_TOI = ( '2010-308T14:01:05.242' ) DIF_TOI = ( '2010-308T13:59:47.310' ) DII_TOI = ( '2005-185T05:44:34.200' ) \begintext " END_OBJECT = DATA_SET_INFORMATION OBJECT = DATA_SET_MISSION MISSION_NAME = "EPOXI" END_OBJECT = DATA_SET_MISSION OBJECT = DATA_SET_TARGET TARGET_NAME = "103P/HARTLEY 2 (1986 E2)" END_OBJECT = DATA_SET_TARGET OBJECT = DATA_SET_TARGET TARGET_NAME = "GJ 436" END_OBJECT = DATA_SET_TARGET OBJECT = DATA_SET_TARGET TARGET_NAME = "HAT-P-4" END_OBJECT = DATA_SET_TARGET OBJECT = DATA_SET_TARGET TARGET_NAME = "HAT-P-7" END_OBJECT = DATA_SET_TARGET OBJECT = DATA_SET_TARGET TARGET_NAME = "TRES-2" END_OBJECT = DATA_SET_TARGET OBJECT = DATA_SET_TARGET TARGET_NAME = "TRES-3" END_OBJECT = DATA_SET_TARGET OBJECT = DATA_SET_TARGET TARGET_NAME = "XO-2" END_OBJECT = DATA_SET_TARGET OBJECT = DATA_SET_TARGET TARGET_NAME = "XO-3" END_OBJECT = DATA_SET_TARGET OBJECT = DATA_SET_TARGET TARGET_NAME = "WASP-3" END_OBJECT = DATA_SET_TARGET OBJECT = DATA_SET_HOST INSTRUMENT_HOST_ID = "DIF" INSTRUMENT_ID = "SPICE" END_OBJECT = DATA_SET_HOST OBJECT = DATA_SET_REFERENCE_INFORMATION REFERENCE_KEY_ID = UNK END_OBJECT = DATA_SET_REFERENCE_INFORMATION END_OBJECT = DATA_SET END