! File: 1184C.PROP ! Database: PEPDB ! Date: 16-FEB-1994:05:05:53 coverpage: title_1: ULTRAVIOLET ATLAS OF BRIGHT, SUITABLE COMET OF OPPORTUNITY sci_cat: SOLAR SYSTEM sci_subcat: COMETS proposal_for: GTO/HRS targ_of_opp: Y pi_fname: JOHN pi_mi: C. pi_lname: BRANDT pi_inst: LASP-UNIVERSITY OF COLORADO pi_country: USA pi_phone: 303-492-3215 hours_pri: 7.10 num_pri: 1 wf_pc: Y fos: Y hrs: Y realtime: Y time_crit: Y ! end of coverpage abstract: line_1: This project is a replacement for the Halley's Comet line_2: observations by the HRS outlined in our original proposal. line_3: Our intention is to select a comet of opportunity that is line_4: bright enough to obtain useful observations in the line_5: ultraviolet and that has an orbit which permits line_6: acquisition and tracking by the Space Telescope over an line_7: extended period of time. The goal is to obtain basically line_8: an HRS atlas concentrating on 20,000 spectral resolution. line_9: The strategy will be to take FOS spectra covering the line_10: entire wavelength region of interest, and then to take HRS line_11: medium and high resolution spectra of specific regions. line_12: The detailed plan for this project depends on the current line_13: capabilities of the HST, and is subject to change. line_14: original limits of GTO time. This is a priority 1 line_15: observing program, cycle TBD. ! ! end of abstract general_form_proposers: lname: BRANDT fname: JOHN title: PI mi: C. inst: LASP-UNIVERSITY OF COLORADO country: USA ! ! end of general_form_proposers block general_form_text: question: 3 section: 1 line_1: The general approach is as follows. First FOS spectra with the line_2: high resolution gratings will be taken to cover the spectral range line_3: from 1150 through 3306 A, with moderate S/N. Then GHRS medium and line_4: high resolution spectra will be taken in various regions of line_5: interest. One of the main goals will be an extended exposure of line_6: the OH/OD 0-0 transition near 3080 A with echelle B. A shorter line_7: exposure here using G270M will be obtained to cover the entire OH line_8: 0-0 band. Lyman alpha will be covered with G160M, and various line_9: other transitions will be covered with other medium resolution line_10: gratings. The target acquisition/tracking procedure is as line_11: follows: A total of 24 HST orbits will be used, divided into 8 line_12: sets of 3 orbits. It is assumed that each orbit has a total of line_13: 52 minutes of charged observing time, bringing the total time for line_14: this proposal to 20.8 hours. In the first orbit of each set line_15: of 3 orbits we will acquire a real-time image using the line_16: WFC F785LP, putting the cometary nucleus into the apex of line_17: chip 2, which should be the most appropriate position for line_18: subsequent transfer to either the FOS/BL or GHRS. We will use line_19: the 4.3" FOS aperture and the 2x2" LSA GHRS aperture for the line_20: subsequent observations. The first two sets of 3 orbits will line_21: be FOS orbits (WFC image followed by 2 FOS orbits), and the next line_22: six sets of 3 orbits will be GHRS orbits (WFC image followed by line_23: 2 GHRS orbits). ! question: 3 section: 2 line_1: With each WFC image orbit (the first of each set of 3) we will line_2: determine a zero-point ephemeris offset, which will be applied to line_3: both subsequent orbits in the set of 3, in order to center the line_4: nucleus in the FOS (or GHRS) aperture. The 2nd and 3rd orbits of line_5: the first set of 3 will be identical and will consist of the line_6: following: (1) Guide star acquisition; (2) Uplink of ephemeris line_7: offset to position comet nucleus in 4.3" FOS aperture; (3) FOS line_8: image to confirm positon of target in 4.3" aperture (note that line_9: if the TDRSS link is still open, we may use it to uplink another line_10: offset if the target is poorly centered at this point); (4) line_11: FOS/BL exposure with grating 130H for the remainder of the orbit line_12: observability window. This exposure is expected to last a line_13: minimum of 16 minutes, yielding 4 spectral readouts of 4-min line_14: exposures. The second and third orbits of the second set of line_15: 3 will be identical to the second and third orbits of the first line_16: set of 3 EXCEPT that in the second orbit of the second set, line_17: grating 190H will be used for the exposure, and in the third line_18: orbit of the second set grating 270H will be used for the line_19: exposure. The second and third orbits of the 6 remaining sets line_20: of 3 orbits will use the GHRS. These orbits will consist of line_21: the following: (1) Guide star acquisition; (2) Uplink of line_22: ephemeris offset to position the comet nucleus in the 2x2" line_23: GHRS LSA; (3) GHRS accum exposure for the remainder of the orbit ! question: 3 section: 3 line_1: observability window (note that it does not make sense to try to line_2: map the aperture in the UV since the cometary UV profile will be line_3: flat and nuclear position will be poorly defined). This should line_4: yield approximately 30 minutes of exposure time per orbit line_5: (assuming about 12.5 min for the GS acq and 8.5 min for the line_6: real-time uplink). The gratings and grating positions used will line_7: depend on the orbit and are delineated below. The observing plan line_8: is summarized by orbit as: line_9: ORBIT 1: WFC image, F785LP; real-time analysis for ephem. offset. line_10: ORBIT 2: GS acq; Uplink ephem. offset; FOS image; 130H exposure. line_11: ORBIT 3: GS acq; Uplink ephem. offset; FOS image; 130H exposure. line_12: ORBIT 4: WFC image, F785LP; real-time analysis for ephem. offset. line_13: ORBIT 5: GS acq; Uplink ephem. offset; FOS image; 190H exposure. line_14: ORBIT 6: GS acq; Uplink ephem. offset; FOS image; 270H exposure. line_15: ORBIT 7: WFC image, F785LP; real-time analysis for ephem. offset. line_16: ORBIT 8: GS acq; Uplink ephem. offset; HRS Ech-B exp, 3080A. line_17: ORBIT 9: GS acq; Uplink ephem. offset; HRS Ech-B exp, 3080A. line_18: ORBIT 10: WFC image, F785LP; INT ACQ for ephem. offset. line_19: ORBIT 11: GS acq; Uplink ephem. offset; HRS Ech-B exp, 3080A. line_20: ORBIT 12: GS acq; Uplink ephem. offset; HRS Ech-B exp, 3080A. line_21: ORBIT 13: WFC image, F785LP; INT ACQ for ephem. offset. line_22: ORBIT 14: GS acq; Uplink ephem. offset; HRS Ech-B exp, 3080A. line_23: ORBIT 15: GS acq; Uplink ephem. offset; HRS Ech-B exp, 3080A. ! question: 3 section: 4 line_1: ORBIT 16: WFC image, F785LP; INT ACQ for ephem. offset. line_2: ORBIT 17: GS acq; Uplink ephem. offset; HRS Ech-B exp, 3080A. line_3: ORBIT 18: GS acq; Uplink ephem. offset; HRS Ech-B, ET=10m, line_4: wave=3085; HRS G160M, ET=20m, wave=1561. (OH, CI) line_5: ORBIT 19: WFC image, F785LP; INT ACQ for ephem. offset. line_6: ORBIT 20: GS acq; Uplink ephem. offset; HRS G270M, ET=5m, line_7: wave=3085; G270M, ET=5m, wave=2576A; G270M, ET=10m, wave=2890A; line_8: G270M, ET=5m, wave=2820; G270M, ET=5m, wave=3142. (OH, CS, CO2+, line_9: OH 1-0, OH 1-1) line_10: ORBIT 21: GS acq; Uplink ephem. offset; HRS G270M, ET=10m, line_11: wave=2321A; HRS G270M, ET=5m, wave=2436A; HRS G270M, ET=15m, line_12: wave=2663; (C2, HI 2nd order, CS) line_13: ORBIT 22: WFC image, F785LP; INT ACQ for ephem. offset. line_14: ORBIT 23: GS acq; Uplink ephem. offset; HRS G200M, ET=10m, line_15: wave=1817A; HRS G200M, ET=20m, wave=2190. (SI, CO+) line_16: ORBIT 24: GS acq; Uplink ephem. offset; HRS G160M, ET=10m, line_17: wave=1216A; HRS G160M, ET=10m, wave=1304A; HRS G160M, ET=10m, line_18: wave=1657A. (Ly-alpha, OI, CI) line_19: Each set of 3 orbits should be performed with a gap of less than line_20: or equal to 1 day before the next set, so that the entire group line_21: of 8 sets (24 orbits) will be executed within the shortest amount line_22: of time possible given the number of RT links available. ! question: 3 section: 5 line_1: The sequences described above assume there will be suitable guide line_2: stars available in each orbit, from which we can switch to gyro line_3: control if the guide star pair is lost due to cometary motion. line_4: However, we have also defined an alternate sequence to be used if line_5: siutable guide stars are not available. This sequence is referred line_6: to as a dummy sequence. In this case, each logsheet line will be line_7: preceded by a dummy guide star acquisition using a nearby fixed line_8: target. This will enable us to transfer to gyro control for the line_9: subsequent comet observations. This will cost an additional line_10: amount of time during each orbit due to the slew time necessary line_11: for transfer from the dummy target to the comet. The general line_12: procedure described above also assumes that HST will not have line_13: guide star hand-off capabilities. If this capability is available line_14: we will use the hand-offs rather than proceeding to gyro control. line_15: In this case, each FOS orbit or GHRS orbit (the 2 orbits line_16: subsequent to the orbit in which the WFC image is taken) will line_17: begin with a guide star RE-acquisition, rather than a guide star line_18: acq. With the time saved during the re-acq, we will subsequently line_19: perform an onboard acq to center the comet in the 4.3 arcsec line_20: aperture if it is an FOS orbit, or increase exposure times if line_21: it is a GHRS orbit. line_22: NOTE ADDED BY SPB: DUMMY exposures were found not to be line_23: necessary, and were removed. ! question: 4 section: 1 line_1: This program requires high sensitivity and high UV spectral line_2: resolution observations of a diffuse cometary source. Only line_3: HST has these capabilities. ! question: 5 section: 1 line_1: These observations are to be made on an unknown comet of line_2: opportunity. A real time uplink will be needed to line_3: position the spectrograph apertures at a known, appropriate line_4: position on the comet to ensure sufficient signal and allow a line_5: clear interpretation of the results. Comet must be observed at line_6: specific positions in its orbit, hence the science observations line_7: are time critical. ! question: 6 section: 1 line_1: N/A. ! question: 7 section: 1 line_1: Observations will be reduced using the facilities of the line_2: Laboratory for Atmospheric and Space Physics and software line_3: developed by the GHRS IDT. ! question: 8 section: 1 line_1: As per previous agreement with STScI, the time allocated to line_2: this program may be utilized after the end of the GTO period if line_3: no suitable comet of opportunity appears during the GTO period. ! question: 9 section: 1 line_1: The only previous HST data were for the GHRS team project on line_2: the quasar 3C 273, and for science verification tests, none of line_3: which are related to this proposal. ! question: 10 section: 1 line_1: VAX computer, IBM-compatible PC, Image display device, line_2: Graduate students, Data reduction software (from HRS IDT). ! !end of general form text general_form_address: lname: BRANDT fname: JOHN mi: C. category: PI inst: UNIVERSITY OF COLORADO addr_1: UNIVERSITY OF COLORADO addr_2: LABORATORY FOR ATMOSPHERIC addr_3: AND SPACE PHYSICS, CB 392 city: BOULDER state: CO zip: 80309 country: USA phone: 303 492 3215 ! ! end of general_form_address records ! No fixed target records found solar_system_targets: targnum: 1 name_1: COMET descr_1: COMET OF-OPORTUNITY lev1_1: TYPE = COMET, lev1_2: Q = 1.202158, E = 0.704849, lev1_3: O = 81.0530, W = 57.4820, lev1_4: I = 11.8458, lev1_5: T = 03-MAR-93:23:03:33, lev1_6: EQUINOX = J2000, lev1_7: EPOCH = 22-FEB-93, ACQ = 0.25 comment_1: GENERIC COMET, FILL IN ACTUAL comment_2: VALUES WHEN AN OPORTUNISTIC comment_3: COMET PRESENTS ITSELF fluxnum_1: 1 fluxval_1: SURF(V) = 14 +/- 1 fluxnum_2: 2 fluxval_2: SURF-LINE(4315) = 2.5 +/- 1.2 E-14 fluxnum_3: 3 fluxval_3: W-LINE(4315) = 0.029 fluxnum_4: 4 fluxval_4: SURF-LINE(5730) = 2 +/- 1 E-14 fluxnum_5: 5 fluxval_5: W-LINE(5730) = 0.038 fluxnum_6: 6 fluxval_6: SURF-LINE(1478) = 2 +/- 1 E-13 fluxnum_7: 7 fluxval_7: W-LINE(1478) = 0.0099 fluxnum_8: 8 fluxval_8: SURF-LINE(2957) = 1.5 +/- 0.7 E-13 fluxnum_9: 9 fluxval_9: W-LINE(2957) = 0.020 fluxnum_10: 10 fluxval_10: SIZE = 1 ! ! end of solar system targets ! No generic target records found exposure_logsheet: linenum: 10.000 sequence_1: DEF sequence_2: ACQ-WFC targname: # config: WFC opmode: IMAGE aperture: WF2 sp_element: F785LP num_exp: 1 time_per_exp: 5.0 S priority: 1 req_1: POS TARG -10, +20 comment_1: WFC IMAGE TO OBTAIN ZERO-PT comment_2: EPHEMERIS OFFSET. TARGET IN comment_3: CHIP 2 APEX. INTERACTIVE ACQ, comment_4: REQUIRES INT ACQ. EXP comment_5: MAY CHANGE DEPENDING ON comment_6: BRIGHTNESS OF COMET. ! linenum: 20.000 sequence_1: DEF sequence_2: ACQ-FOS targname: # config: FOS/BL opmode: ACQ/BINARY aperture: 4.3 sp_element: MIRROR num_exp: 1 time_per_exp: 1 S priority: 1 comment_1: ONBOARD ACQ TO BE USED comment_2: IF GS HANDOFFS AVAILABLE. ! linenum: 30.000 sequence_1: DEF sequence_2: IMAGE-FOS targname: # config: FOS/BL opmode: ACQ aperture: 4.3 sp_element: MIRROR num_exp: 1 time_per_exp: 1 S priority: 1 comment_1: IMAGE OF APERTURE TO CONFIRM comment_2: TARGET POSITION. ! linenum: 31.000 sequence_1: DEF sequence_2: IMAGE-FOS1 targname: # config: FOS/BL opmode: ACQ aperture: 4.3 sp_element: MIRROR num_exp: 1 time_per_exp: 1 S priority: 1 comment_1: IMAGE OF APERTURE TO CONFIRM comment_2: TARGET POSITION. ! linenum: 40.000 sequence_1: DEF sequence_2: FOS-130 targname: # config: FOS/BL opmode: ACCUM aperture: 4.3 sp_element: G130H num_exp: 1 time_per_exp: 16M priority: 1 comment_1: EXPOSE FOR AS MUCH TIME comment_2: AS IS LEFT IN ORBIT AFTER comment_3: GS ACQ AND FOS IMAGE. IF GS PAIR comment_4: IS LOST, SWITCH TO GYROS. ASSUMES comment_5: 52-MINUTE OBSERVING WINDOW. ! linenum: 50.000 sequence_1: DEF sequence_2: FOS-190 targname: # config: FOS/BL opmode: ACCUM aperture: 4.3 sp_element: G190H num_exp: 1 time_per_exp: 16M priority: 1 comment_1: EXPOSE FOR AS MUCH TIME comment_2: AS IS LEFT IN ORBIT AFTER comment_3: GS ACQ AND FOS IMAGE. IF GS PAIR comment_4: IS LOST, SWITCH TO GYROS. ASSUMES comment_5: 52-MINUTE OBSERVING WINDOW. ! linenum: 60.000 sequence_1: DEF sequence_2: FOS-270 targname: # config: FOS/BL opmode: ACCUM aperture: 4.3 sp_element: G270H num_exp: 1 time_per_exp: 16M priority: 1 comment_1: EXPOSE FOR AS MUCH TIME comment_2: AS IS LEFT IN ORBIT AFTER comment_3: GS ACQ AND FOS IMAGE. IF GS PAIR comment_4: IS LOST, SWITCH TO GYROS. ASSUMES comment_5: 52-MINUTE OBSERVING WINDOW. ! linenum: 70.000 sequence_1: DEF sequence_2: HRS-OD targname: # config: HRS opmode: ACCUM aperture: 2.0 sp_element: ECH-B wavelength: 3079 num_exp: 3 time_per_exp: 10 M fluxnum_1: 2 priority: 1 param_1: FP-SPLIT=STD comment_1: SWITCH TO GYROS IF GS LOST. comment_2: EXPOSE AFTER GS ACQ AND comment_3: EPHEMERIS OFFSET UPLINK. comment_4: ASSUMES 52-MINUTE OBSERVING comment_5: WINDOW, 12.5M FOR GS ACQ AND comment_6: 8.5M FOR UPLINK. ! linenum: 80.000 sequence_1: DEF sequence_2: HRS-O18 targname: # config: HRS opmode: ACCUM aperture: 2.0 sp_element: ECH-B wavelength: 3085 num_exp: 1 time_per_exp: 10 M s_to_n: 100 fluxnum_1: 3 priority: 1 param_1: FP-SPLIT=STD comment_1: SWITCH TO GYROS IF GS LOST. comment_2: EXPOSE AFTER GS ACQ AND comment_3: EPHEMERIS OFFSET UPLINK. comment_4: ORBIT 18. ! linenum: 90.000 sequence_1: DEF sequence_2: HRS-O18 targname: # config: HRS opmode: ACCUM aperture: 2.0 sp_element: G160M wavelength: 1561 num_exp: 2 time_per_exp: 10 M s_to_n: 6 fluxnum_1: 4 priority: 1 param_1: FP-SPLIT=STD comment_1: SWITCH TO GYROS IF GS LOST. comment_2: EXPOSE AFTER GS ACQ AND comment_3: EPHEMERIS OFFSET UPLINK. comment_4: ORBIT 18. ! linenum: 100.000 sequence_1: DEF sequence_2: HRS-O20 targname: # config: HRS opmode: ACCUM aperture: 2.0 sp_element: G270M wavelength: 3085 num_exp: 1 time_per_exp: 5 M s_to_n: 100 fluxnum_1: 3 priority: 1 param_1: FP-SPLIT=STD comment_1: SWITCH TO GYROS IF GS LOST. comment_2: EXPOSE AFTER GS ACQ AND comment_3: EPHEMERIS OFFSET UPLINK. comment_4: ORBIT 20. ! linenum: 110.000 sequence_1: DEF sequence_2: HRS-O20 targname: # config: HRS opmode: ACCUM aperture: 2.0 sp_element: G270M wavelength: 2576 num_exp: 1 time_per_exp: 5 M s_to_n: 10 fluxnum_1: 5 priority: 1 param_1: FP-SPLIT=STD comment_1: SWITCH TO GYROS IF GS LOST. comment_2: EXPOSE AFTER GS ACQ AND comment_3: EPHEMERIS OFFSET UPLINK. comment_4: ORBIT 20. ! linenum: 120.000 sequence_1: DEF sequence_2: HRS-O20 targname: # config: HRS opmode: ACCUM aperture: 2.0 sp_element: G270M wavelength: 2890 num_exp: 1 time_per_exp: 10 M s_to_n: 10 fluxnum_1: 6 priority: 1 param_1: FP-SPLIT=STD comment_1: SWITCH TO GYROS IF GS LOST. comment_2: EXPOSE AFTER GS ACQ AND comment_3: EPHEMERIS OFFSET UPLINK. comment_4: ORBIT 20. ! linenum: 130.000 sequence_1: DEF sequence_2: HRS-O20 targname: # config: HRS opmode: ACCUM aperture: 2.0 sp_element: G270M wavelength: 2820 num_exp: 1 time_per_exp: 5 M s_to_n: 30 fluxnum_1: 7 priority: 1 param_1: FP-SPLIT=STD comment_1: SWITCH TO GYROS IF GS LOST. comment_2: EXPOSE AFTER GS ACQ AND comment_3: EPHEMERIS OFFSET UPLINK. comment_4: ORBIT 20. ! linenum: 140.000 sequence_1: DEF sequence_2: HRS-O20 targname: # config: HRS opmode: ACCUM aperture: 2.0 sp_element: G270M wavelength: 3142 num_exp: 1 time_per_exp: 5 M s_to_n: 15 fluxnum_1: 8 priority: 1 param_1: FP-SPLIT=STD comment_1: SWITCH TO GYROS IF GS LOST. comment_2: EXPOSE AFTER GS ACQ AND comment_3: EPHEMERIS OFFSET UPLINK. comment_4: ORBIT 20. ! linenum: 150.000 sequence_1: DEF sequence_2: HRS-O21 targname: # config: HRS opmode: ACCUM aperture: 2.0 sp_element: G270M wavelength: 2321 num_exp: 1 time_per_exp: 10 M s_to_n: 6 fluxnum_1: 9 priority: 1 param_1: FP-SPLIT=STD comment_1: SWITCH TO GYROS IF GS LOST. comment_2: EXPOSE AFTER GS ACQ AND comment_3: EPHEMERIS OFFSET UPLINK. comment_4: ORBIT 21. ! linenum: 160.000 sequence_1: DEF sequence_2: HRS-O21 targname: # config: HRS opmode: ACCUM aperture: 2.0 sp_element: G270M wavelength: 2436 num_exp: 1 time_per_exp: 5 M s_to_n: 8 priority: 1 param_1: FP-SPLIT=STD comment_1: SWITCH TO GYROS IF GS LOST. comment_2: EXPOSE AFTER GS ACQ AND comment_3: EPHEMERIS OFFSET UPLINK. comment_4: ORBIT 21. ! linenum: 170.000 sequence_1: DEF sequence_2: HRS-O21 targname: # config: HRS opmode: ACCUM aperture: 2.0 sp_element: G270M wavelength: 2663 num_exp: 2 time_per_exp: 7.5 M s_to_n: 6 priority: 1 param_1: FP-SPLIT=STD comment_1: SWITCH TO GYROS IF GS LOST. comment_2: EXPOSE AFTER GS ACQ AND comment_3: EPHEMERIS OFFSET UPLINK. comment_4: ORBIT 21. ! linenum: 180.000 sequence_1: DEF sequence_2: HRS-O23 targname: # config: HRS opmode: ACCUM aperture: 2.0 sp_element: G200M wavelength: 1817 num_exp: 1 time_per_exp: 10 M s_to_n: 9 priority: 1 param_1: FP-SPLIT=STD comment_1: SWITCH TO GYROS IF GS LOST. comment_2: EXPOSE AFTER GS ACQ AND comment_3: EPHEMERIS OFFSET UPLINK. comment_4: ORBIT 23. ! linenum: 190.000 sequence_1: DEF sequence_2: HRS-O23 targname: # config: HRS opmode: ACCUM aperture: 2.0 sp_element: G200M wavelength: 2190 num_exp: 2 time_per_exp: 10 M s_to_n: 5 priority: 1 param_1: FP-SPLIT=STD comment_1: SWITCH TO GYROS IF GS LOST. comment_2: EXPOSE AFTER GS ACQ AND comment_3: EPHEMERIS OFFSET UPLINK. comment_4: ORBIT 23. ! linenum: 200.000 sequence_1: DEF sequence_2: HRS-O24 targname: # config: HRS opmode: ACCUM aperture: 2.0 sp_element: G160M wavelength: 1216 num_exp: 2 time_per_exp: 5 M s_to_n: 100 priority: 1 param_1: FP-SPLIT=STD comment_1: SWITCH TO GYROS IF GS LOST. comment_2: EXPOSE AFTER GS ACQ AND comment_3: EPHEMERIS OFFSET UPLINK. comment_4: ORBIT 24. ! linenum: 203.000 sequence_1: DEF sequence_2: HRS-O24 targname: # config: HRS opmode: ACCUM aperture: 2.0 sp_element: G160M wavelength: 1304 num_exp: 1 time_per_exp: 10 M s_to_n: 12 priority: 1 param_1: FP-SPLIT=STD comment_1: SWITCH TO GYROS IF GS LOST. comment_2: EXPOSE AFTER GS ACQ AND comment_3: EPHEMERIS OFFSET UPLINK. comment_4: ORBIT 24. ! linenum: 204.000 sequence_1: DEF sequence_2: HRS-O24 targname: # config: HRS opmode: ACCUM aperture: 2.0 sp_element: G160M wavelength: 1657 num_exp: 1 time_per_exp: 10 M s_to_n: 12 priority: 1 param_1: FP-SPLIT=STD comment_1: SWITCH TO GYROS IF GS LOST. comment_2: EXPOSE AFTER GS ACQ AND comment_3: EPHEMERIS OFFSET UPLINK. comment_4: ORBIT 24. ! linenum: 205.000 sequence_1: USE sequence_2: ACQ-WFC targname: COMET req_1: INT ACQ FOR 215-225; req_2: SEQ 205-225 NO GAP; req_3: SELECT 1 OF 205-250 OR 255-300; req_4: COND IF M2 < 9.8 / 205-250; req_5: CRIT OBS / 205-250; req_6: CYCLE 2 / 205-250; req_7: GUIDE TOL 0.6" / 205-250; comment_1: WFC IMAGE TO GET ZERO-PT EPHEMERIS comment_2: FOR NEXT TWO OFFSET. INT-ACQ comment_3: ORBITS IN WHICH FOS MAP AND comment_4: ACCUMS TAKEN. THIS IS 1ST ORBIT. comment_5: SELECT THIS SET IF NUCLEAR comment_6: MAG BRIGHTER THAN 9.8. ! linenum: 215.000 sequence_1: USE sequence_2: FOS-130 targname: COMET req_1: REQ UPLINK; comment_1: SPECTRAL EXPOSURE FOR comment_2: 2ND ORBIT. ! linenum: 225.000 sequence_1: USE sequence_2: FOS-130 targname: COMET req_1: REQ UPLINK; comment_1: SPECTRAL EXPOSURE FOR comment_2: 3RD ORBIT. ! linenum: 230.000 sequence_1: USE sequence_2: ACQ-WFC targname: COMET req_1: INT ACQ FOR 240-250; req_2: SEQ 230-250 NO GAP comment_1: WFC IMAGE TO GET ZERO-PT comment_2: EPHEMERIS OFFSET. INT-ACQ comment_3: FOR NEXT TWO ORBITS IN comment_4: WHICH FOS MAP AND ACCUMS comment_5: TAKEN. THIS IS 4TH ORBIT. ! linenum: 240.000 sequence_1: USE sequence_2: FOS-190 targname: COMET req_1: REQ UPLINK; comment_1: SPECTRAL EXPOSURE FOR comment_2: 5TH ORBIT. ! linenum: 250.000 sequence_1: USE sequence_2: FOS-270 targname: COMET req_1: REQ UPLINK; comment_1: SPECTRAL EXPOSURE FOR comment_2: 6TH ORBIT. ! linenum: 255.000 sequence_1: USE sequence_2: ACQ-WFC targname: COMET req_1: INT ACQ FOR 260-275; req_2: SEQ 255-275 NO GAP; req_3: CRIT OBS / 255-300; req_4: CYCLE 2 / 255-300; req_5: GUIDE TOL 0.6" / 255-300; req_6: COND IF M2 > 9.8 / 255-300; comment_1: WFC IMAGE TO GET ZERO-PT EPHEMERIS comment_2: FOR NEXT TWO OFFSET. INT-ACQ comment_3: ORBITS IN WHICH FOS MAP AND comment_4: ACCUMS TAKEN. THIS IS 1ST ORBIT. comment_5: SELECT THIS SET IF NUCLEAR comment_6: MAG FAINTER THAN 9.8. ! linenum: 260.000 sequence_1: USE sequence_2: IMAGE-FOS targname: COMET req_1: REQ UPLINK; req_2: SEQ 260-265 NON-INT comment_1: FOS APERTURE MAP FOR comment_2: 2ND ORBIT ! linenum: 265.000 sequence_1: USE sequence_2: FOS-130 targname: COMET comment_1: SPECTRAL EXPOSURE FOR comment_2: 2ND ORBIT. ! linenum: 270.000 sequence_1: USE sequence_2: IMAGE-FOS1 targname: COMET req_1: REQ UPLINK; req_2: SEQ 270-275 NON-INT comment_1: FOS APERTURE MAP FOR comment_2: 3RD ORBIT ! linenum: 275.000 sequence_1: USE sequence_2: FOS-130 targname: COMET comment_1: SPECTRAL EXPOSURE FOR comment_2: 3RD ORBIT. ! linenum: 280.000 sequence_1: USE sequence_2: ACQ-WFC targname: COMET req_1: INT ACQ FOR 285-300; req_2: SEQ 280-300 NO GAP comment_1: WFC IMAGE TO GET ZERO-PT comment_2: EPHEMERIS OFFSET. INT-ACQ comment_3: FOR NEXT TWO ORBITS IN comment_4: WHICH FOS MAP AND ACCUMS comment_5: TAKEN. THIS IS 4TH ORBIT. ! linenum: 285.000 sequence_1: USE sequence_2: IMAGE-FOS targname: COMET req_1: REQ UPLINK; req_2: SEQ 285-290 NON-INT comment_1: FOS APERTURE MAP FOR comment_2: 5TH ORBIT ! linenum: 290.000 sequence_1: USE sequence_2: FOS-190 targname: COMET comment_1: SPECTRAL EXPOSURE FOR comment_2: 5TH ORBIT. ! linenum: 295.000 sequence_1: USE sequence_2: IMAGE-FOS1 targname: COMET req_1: REQ UPLINK; req_2: SEQ 295-300 NON-INT comment_1: FOS APERTURE MAP FOR comment_2: 6TH ORBIT ! linenum: 300.000 sequence_1: USE sequence_2: FOS-270 targname: COMET comment_1: SPECTRAL EXPOSURE FOR comment_2: 6TH ORBIT. ! linenum: 310.000 sequence_1: USE sequence_2: ACQ-WFC targname: COMET req_1: INT ACQ FOR 320-330; req_2: SEQ 310-330 NO GAP; req_3: CRIT OBS / 310-480; req_4: GUIDE TOL 0.6" / 310-480; req_6: CYCLE 2 / 310-480; comment_1: WFC IMAGE TO GET ZERO-PT comment_2: EPHEMERIS OFFSET. INT-ACQ comment_3: FOR NEXT TWO ORBITS IN comment_4: WHICH GHRS ACCUMS TAKEN. comment_5: THIS IS 7TH ORBIT. ! linenum: 320.000 sequence_1: USE sequence_2: HRS-OD targname: COMET req_1: REQ UPLINK; comment_1: SPECTRAL EXPOSURE FOR comment_2: 8TH ORBIT. DONE AFTER comment_3: GS ACQ AND UPLINK. ! linenum: 330.000 sequence_1: USE sequence_2: HRS-OD targname: COMET req_1: REQ UPLINK; comment_1: SPECTRAL EXPOSURE FOR comment_2: 9TH ORBIT. DONE AFTER comment_3: GS ACQ AND UPLINK. ! linenum: 340.000 sequence_1: USE sequence_2: ACQ-WFC targname: COMET req_1: INT ACQ FOR 350-360; req_2: SEQ 340-360 NO GAP comment_1: WFC IMAGE TO GET ZERO-PT comment_2: EPHEMERIS OFFSET. INT-ACQ comment_3: FOR NEXT TWO ORBITS IN comment_4: WHICH GHRS ACCUMS TAKEN. comment_5: THIS IS 10TH ORBIT. ! linenum: 350.000 sequence_1: USE sequence_2: HRS-OD targname: COMET req_1: REQ UPLINK; comment_1: SPECTRAL EXPOSURE FOR comment_2: 11TH ORBIT. DONE AFTER comment_3: GS ACQ AND UPLINK. ! linenum: 360.000 sequence_1: USE sequence_2: HRS-OD targname: COMET req_1: REQ UPLINK; comment_1: SPECTRAL EXPOSURE FOR comment_2: 12TH ORBIT. DONE AFTER comment_3: GS ACQ AND UPLINK. ! linenum: 370.000 sequence_1: USE sequence_2: ACQ-WFC targname: COMET req_1: INT ACQ FOR 380-390; req_2: SEQ 370-390 NO GAP comment_1: WFC IMAGE TO GET ZERO-PT comment_2: EPHEMERIS OFFSET. INT-ACQ comment_3: FOR NEXT TWO ORBITS IN comment_4: WHICH GHRS ACCUMS TAKEN. comment_5: THIS IS 13TH ORBIT. ! linenum: 380.000 sequence_1: USE sequence_2: HRS-OD targname: COMET req_1: REQ UPLINK; comment_1: SPECTRAL EXPOSURE FOR comment_2: 14TH ORBIT. DONE AFTER comment_3: GS ACQ AND UPLINK. ! linenum: 390.000 sequence_1: USE sequence_2: HRS-OD targname: COMET req_1: REQ UPLINK; comment_1: SPECTRAL EXPOSURE FOR comment_2: 15TH ORBIT. DONE AFTER comment_3: GS ACQ AND UPLINK. ! linenum: 400.000 sequence_1: USE sequence_2: ACQ-WFC targname: COMET req_1: INT ACQ FOR 410-420; req_2: SEQ 400-420 NO GAP comment_1: WFC IMAGE TO GET ZERO-PT comment_2: EPHEMERIS OFFSET. INT-ACQ comment_3: FOR NEXT TWO ORBITS IN comment_4: WHICH GHRS ACCUMS TAKEN. comment_5: THIS IS 16TH ORBIT. ! linenum: 410.000 sequence_1: USE sequence_2: HRS-OD targname: COMET req_1: REQ UPLINK; comment_1: SPECTRAL EXPOSURE FOR comment_2: 17TH ORBIT. DONE AFTER comment_3: GS ACQ AND UPLINK. ! linenum: 420.000 sequence_1: USE sequence_2: HRS-O18 targname: COMET req_1: REQ UPLINK; comment_1: SPECTRAL EXPOSURES FOR comment_2: 18TH ORBIT. DONE AFTER comment_3: GS ACQ AND UPLINK. ! linenum: 430.000 sequence_1: USE sequence_2: ACQ-WFC targname: COMET req_1: INT ACQ FOR 440-450; req_2: SEQ 430-450 NO GAP comment_1: WFC IMAGE TO GET ZERO-PT comment_2: EPHEMERIS OFFSET. INT-ACQ comment_3: FOR NEXT TWO ORBITS IN comment_4: WHICH GHRS ACCUMS TAKEN. comment_5: THIS IS 19TH ORBIT. ! linenum: 440.000 sequence_1: USE sequence_2: HRS-O20 targname: COMET req_1: REQ UPLINK; comment_1: SPECTRAL EXPOSURES FOR comment_2: 20TH ORBIT. DONE AFTER comment_3: GS ACQ AND UPLINK. ! linenum: 450.000 sequence_1: USE sequence_2: HRS-O21 targname: COMET req_1: REQ UPLINK; comment_1: SPECTRAL EXPOSURES FOR comment_2: 21TH ORBIT. DONE AFTER comment_3: GS ACQ AND UPLINK. ! linenum: 460.000 sequence_1: USE sequence_2: ACQ-WFC targname: COMET req_1: INT ACQ FOR 470-480; req_2: SEQ 460-480 NO GAP comment_1: WFC IMAGE TO GET ZERO-PT comment_2: EPHEMERIS OFFSET. INT-ACQ comment_3: FOR NEXT TWO ORBITS IN comment_4: WHICH GHRS ACCUMS TAKEN. comment_5: THIS IS 22ND ORBIT. ! linenum: 470.000 sequence_1: USE sequence_2: HRS-O23 targname: COMET req_1: REQ UPLINK; comment_1: SPECTRAL EXPOSURE FOR comment_2: 23RD ORBIT. DONE AFTER comment_3: GS ACQ AND UPLINK. ! linenum: 480.000 sequence_1: USE sequence_2: HRS-O24 targname: COMET req_1: REQ UPLINK; comment_1: SPECTRAL EXPOSURE FOR comment_2: 24TH ORBIT. DONE AFTER comment_3: GS ACQ AND UPLINK. ! ! end of exposure logsheet ! No scan data records found