Proposal 13318 (STScI Edit Number: 0, Created: Thursday, July 11, 2013 1:55:18 PM EST) - Overview
13318 - Giant impacts on giant planets
Cycle: 21, Proposal Category: GO
(UV Initiative)
(Availability Mode: SUPPORTED)
INVESTIGATORS
Name
Prof. Imke de Pater (PI) (Contact)
Dr. Michael H. Wong (CoI) (AdminUSPI) (Contact)
Dr. Heidi B. Hammel (CoI)
Prof. John T. Clarke (CoI)
Dr. Amy Simon-Miller (CoI)
Dr. Agustin Sanchez-Lavega (CoI) (ESA Member)
Dr. Glenn S. Orton (CoI)
Institution
University of California - Berkeley
University of California - Berkeley
Space Science Institute
Boston University
NASA Goddard Space Flight Center
Universidad del Pais Vasco
Jet Propulsion Laboratory
E-Mail
imke@berkeley.edu
mikewong@astro.berkeley.edu
hbh@alum.mit.edu
jclarke@bu.edu
amy.simon@nasa.gov
wupsalaa@bi.ehu.es
go@scn.jpl.nasa.gov
VISITS
Visit Targets used in Visit
Configurations used in Visit
Orbits Used Last Orbit Planner Run
01
(2) SATURN-IMPACT-SITE
WFC3/UVIS
1
11-Jul-2013 14:54:44.0
OP Current
with Visit?
yes
02
(2) SATURN-IMPACT-SITE
WFC3/UVIS
1
11-Jul-2013 14:54:53.0
yes
03
(1) JUPITER-IMPACT-SITE
WFC3/UVIS
1
11-Jul-2013 14:55:02.0
yes
04
(1) JUPITER-IMPACT-SITE
WFC3/UVIS
1
11-Jul-2013 14:55:10.0
yes
4 Total Orbits Used
ABSTRACT
1
Proposal 13318 (STScI Edit Number: 0, Created: Thursday, July 11, 2013 1:55:18 PM EST) - Overview
The 2009 impact and recent superbolides on Jupiter caught the world by surprise and cast doubt on impactor flux estimates for the outer solar system.
Enhanced amateur planetary imaging techniques yield both high spatial resolution (enabling the 2009 impact debris field detection) and rapid frame
rates (enabling the 2010/2012 impact flash detections and lightcurve measurements).
We propose a ToO program to image future impacts on Jupiter and Saturn. To remove the possibility of impact cloud non-detections, the program
will be triggered only if an existing impact debris field is seen, an object on a collision course with Jupiter or Saturn is discovered, or an impact light
curve is measured with an estimated total energy large enough to generate an impact cloud in a giant planet atmosphere (10^20 J).
HST provides the only way to image these events in the ultraviolet, providing information on aerosol altitudes and on smaller particles that are less
visible to ground-based infrared observations. High-resolution imaging with proper timing (not achievable from the ground) is required to measure
precisely both the velocity fields of impact sites and the optical spectrum of impact debris. HST observations of past impacts on Jupiter have also
served both as cornerstones of science investigations at other wavelengths and as vehicles for effective public outreach.
Large outer solar system impacts are governed by the same physics as in the terrestrial events that dominate the impact threat to humans. Studying
the behavior of impactors of various sizes and compositions, as they enter the atmosphere at varying angles and speeds, will better quantify terrestrial
impact hazards.
OBSERVING DESCRIPTION
Observe impact site on target after an impact has been predicted or observed. Target may be Jupiter or Saturn.
Quad subarray (2k x 2k) UVIS imaging data will be acquired in quadrants A and D, due to location of important methane-band filters.
An event will trigger 2 visits, with visit #2 following visit #1 by one target planet rotation (i.e., 6 orbits later for Jupiter or 7 orbits later for Saturn).
Because we include visits to cover both Jupiter and Saturn cases, there are 4 visits in the Phase II even though we were awarded only 2 orbits.
Exposure times must be adjusted once the impact is known, to scale with planetary brightness as the target's heliocentric distance changes over time.
2
Solar System Targets
Visit
Proposal 13318 - SAT-1 (01) - Giant impacts on giant planets
Proposal 13318, SAT-1 (01), implementation
Diagnostic Status: No Diagnostics
Scientific Instruments: WFC3/UVIS
Special Requirements: PCS MODE FINE; DROP TO GYRO IF NECESSARY NO REACQ; GYRO MODE 3GOBAD
Comments: saturn visit #1 of 2
Thu Jul 11 18:55:18 GMT 2013
NOTE: Date of impact is unknown, so duration of visibilities cannot be predicted at this time. When observations are actually planned, we intend to duplicate or eliminate some exposures to fill the available visibility.
Current visit design is for 50-min visibility window.
#
Name
Level 1
Level 2
Level 3
Window
Ephem Center
(2)
SATURN-IMPACT- STD=SATURN
TYPE=PGRAPHIC,LONG=0,LAT=0
SEP OF SATURN-IMPACT-SITE
EARTH
SITE
RHEA FROM EARTH GT 19",
SEP OF SATURN-IMPACT-SITE
TITAN FROM EARTH GT 19"
Comments: NEED TO REFINE LEVEL 2 COORDINATES AFTER IMPACT TAKES PLACE (or after impact location is predicted prior to impact)
3
Proposal 13318 - SAT-1 (01) - Giant impacts on giant planets
Exposures
#
1
Label
Target
Config,Mode,Aperture
FQ889N--A (2) SATURN-IMPA WFC3/UVIS, ACCUM,
CT-SITE
UVIS-QUAD-SUB
Spectral Els.
FQ889N
Opt. Params.
CR-SPLIT=NO
Special Reqs.
Groups
Exp. Time (Total)/[Actual Dur.]
300 Secs (300 Secs)
[==>]
Orbit
[1]
Comments: EXPOSURE TIMES MUST BE REFINED !!
exposure time here is preliminary because target's heliocentric distance at time of observations is not known. once the timing of the impact is known, exposure times must be adjusted to maximize s/n ratio, avoid satura
tion, and optimize observational efficiency.
2
F275W--A (2) SATURN-IMPA WFC3/UVIS, ACCUM,
F275W
CR-SPLIT=NO
140 Secs (140 Secs)
CT-SITE
UVIS1-2K2A-SUB
[==>]
[1]
Comments: EXPOSURE TIMES MUST BE REFINED !!
exposure time here is preliminary because target's heliocentric distance at time of observations is not known. once the timing of the impact is known, exposure times must be adjusted to maximize s/n ratio, avoid satura
tion, and optimize observational efficiency.
3
F631N--A
(2) SATURN-IMPA WFC3/UVIS, ACCUM,
F631N
CR-SPLIT=NO
14 Secs (14 Secs)
CT-SITE
UVIS1-2K2A-SUB
[==>]
[1]
Comments: EXPOSURE TIMES MUST BE REFINED !!
exposure time here is preliminary because target's heliocentric distance at time of observations is not known. once the timing of the impact is known, exposure times must be adjusted to maximize s/n ratio, avoid satura
tion, and optimize observational efficiency.
4
F502N--A
(2) SATURN-IMPA WFC3/UVIS, ACCUM,
F502N
CR-SPLIT=NO
12 Secs (12 Secs)
CT-SITE
UVIS1-2K2A-SUB
[==>]
[1]
Comments: EXPOSURE TIMES MUST BE REFINED !!
exposure time here is preliminary because target's heliocentric distance at time of observations is not known. once the timing of the impact is known, exposure times must be adjusted to maximize s/n ratio, avoid satura
tion, and optimize observational efficiency.
5
F343N--A
(2) SATURN-IMPA WFC3/UVIS, ACCUM,
F343N
CR-SPLIT=NO
20 Secs (20 Secs)
CT-SITE
UVIS1-2K2A-SUB
[==>]
[1]
Comments: EXPOSURE TIMES MUST BE REFINED !!
exposure time here is preliminary because target's heliocentric distance at time of observations is not known. once the timing of the impact is known, exposure times must be adjusted to maximize s/n ratio, avoid satura
tion, and optimize observational efficiency.
6
F225W--A (2) SATURN-IMPA WFC3/UVIS, ACCUM,
F225W
CR-SPLIT=NO
300 Secs (300 Secs)
CT-SITE
UVIS1-2K2A-SUB
[==>]
[1]
Comments: EXPOSURE TIMES MUST BE REFINED !!
exposure time here is preliminary because target's heliocentric distance at time of observations is not known. once the timing of the impact is known, exposure times must be adjusted to maximize s/n ratio, avoid satura
tion, and optimize observational efficiency.
7
FQ889N--A (2) SATURN-IMPA WFC3/UVIS, ACCUM,
FQ889N
CR-SPLIT=NO
300 Secs (300 Secs)
CT-SITE
UVIS-QUAD-SUB
[==>]
[1]
Comments: EXPOSURE TIMES MUST BE REFINED !!
exposure time here is preliminary because target's heliocentric distance at time of observations is not known. once the timing of the impact is known, exposure times must be adjusted to maximize s/n ratio, avoid satura
tion, and optimize observational efficiency.
8
FQ727N--D (2) SATURN-IMPA WFC3/UVIS, ACCUM,
FQ727N
CR-SPLIT=NO
30 Secs (30 Secs)
CT-SITE
UVIS-QUAD-SUB
[==>]
[1]
Comments: EXPOSURE TIMES MUST BE REFINED !!
exposure time here is preliminary because target's heliocentric distance at time of observations is not known. once the timing of the impact is known, exposure times must be adjusted to maximize s/n ratio, avoid satura
tion, and optimize observational efficiency.
4
Orbit Structure
Proposal 13318 - SAT-1 (01) - Giant impacts on giant planets
5
Solar System Targets
Visit
Proposal 13318 - SAT-2 (02) - Giant impacts on giant planets
Proposal 13318, SAT-2 (02), implementation
Diagnostic Status: No Diagnostics
Scientific Instruments: WFC3/UVIS
Special Requirements: PCS MODE FINE; DROP TO GYRO IF NECESSARY NO REACQ; GYRO MODE 3GOBAD; AFTER 01 BY 6 Orbits TO 7 Orbits
Comments: saturn visit #2 of 2
Thu Jul 11 18:55:21 GMT 2013
NOTE: Date of impact is unknown, so duration of visibilities cannot be predicted at this time. When observations are actually planned, we intend to duplicate or eliminate some exposures to fill the available visibility.
Current visit design is for 50-min visibility window.
#
Name
Level 1
Level 2
Level 3
Window
Ephem Center
(2)
SATURN-IMPACT- STD=SATURN
TYPE=PGRAPHIC,LONG=0,LAT=0
SEP OF SATURN-IMPACT-SITE
EARTH
SITE
RHEA FROM EARTH GT 19",
SEP OF SATURN-IMPACT-SITE
TITAN FROM EARTH GT 19"
Comments: NEED TO REFINE LEVEL 2 COORDINATES AFTER IMPACT TAKES PLACE (or after impact location is predicted prior to impact)
6
Proposal 13318 - SAT-2 (02) - Giant impacts on giant planets
Exposures
#
1
Label
Target
Config,Mode,Aperture
FQ889N--A (2) SATURN-IMPA WFC3/UVIS, ACCUM,
CT-SITE
UVIS-QUAD-SUB
Spectral Els.
FQ889N
Opt. Params.
CR-SPLIT=NO
Special Reqs.
Groups
Exp. Time (Total)/[Actual Dur.]
300 Secs (300 Secs)
[==>]
Orbit
[1]
Comments: EXPOSURE TIMES MUST BE REFINED !!
exposure time here is preliminary because target's heliocentric distance at time of observations is not known. once the timing of the impact is known, exposure times must be adjusted to maximize s/n ratio, avoid satura
tion, and optimize observational efficiency.
2
F275W--A (2) SATURN-IMPA WFC3/UVIS, ACCUM,
F275W
CR-SPLIT=NO
140 Secs (140 Secs)
CT-SITE
UVIS1-2K2A-SUB
[==>]
[1]
Comments: EXPOSURE TIMES MUST BE REFINED !!
exposure time here is preliminary because target's heliocentric distance at time of observations is not known. once the timing of the impact is known, exposure times must be adjusted to maximize s/n ratio, avoid satura
tion, and optimize observational efficiency.
3
F631N--A
(2) SATURN-IMPA WFC3/UVIS, ACCUM,
F631N
CR-SPLIT=NO
14 Secs (14 Secs)
CT-SITE
UVIS1-2K2A-SUB
[==>]
[1]
Comments: EXPOSURE TIMES MUST BE REFINED !!
exposure time here is preliminary because target's heliocentric distance at time of observations is not known. once the timing of the impact is known, exposure times must be adjusted to maximize s/n ratio, avoid satura
tion, and optimize observational efficiency.
4
F502N--A
(2) SATURN-IMPA WFC3/UVIS, ACCUM,
F502N
CR-SPLIT=NO
12 Secs (12 Secs)
CT-SITE
UVIS1-2K2A-SUB
[==>]
[1]
Comments: EXPOSURE TIMES MUST BE REFINED !!
exposure time here is preliminary because target's heliocentric distance at time of observations is not known. once the timing of the impact is known, exposure times must be adjusted to maximize s/n ratio, avoid satura
tion, and optimize observational efficiency.
5
F343N--A
(2) SATURN-IMPA WFC3/UVIS, ACCUM,
F343N
CR-SPLIT=NO
20 Secs (20 Secs)
CT-SITE
UVIS1-2K2A-SUB
[==>]
[1]
Comments: EXPOSURE TIMES MUST BE REFINED !!
exposure time here is preliminary because target's heliocentric distance at time of observations is not known. once the timing of the impact is known, exposure times must be adjusted to maximize s/n ratio, avoid satura
tion, and optimize observational efficiency.
6
F225W--A (2) SATURN-IMPA WFC3/UVIS, ACCUM,
F225W
CR-SPLIT=NO
300 Secs (300 Secs)
CT-SITE
UVIS1-2K2A-SUB
[==>]
[1]
Comments: EXPOSURE TIMES MUST BE REFINED !!
exposure time here is preliminary because target's heliocentric distance at time of observations is not known. once the timing of the impact is known, exposure times must be adjusted to maximize s/n ratio, avoid satura
tion, and optimize observational efficiency.
7
FQ889N--A (2) SATURN-IMPA WFC3/UVIS, ACCUM,
FQ889N
CR-SPLIT=NO
300 Secs (300 Secs)
CT-SITE
UVIS-QUAD-SUB
[==>]
[1]
Comments: EXPOSURE TIMES MUST BE REFINED !!
exposure time here is preliminary because target's heliocentric distance at time of observations is not known. once the timing of the impact is known, exposure times must be adjusted to maximize s/n ratio, avoid satura
tion, and optimize observational efficiency.
8
FQ727N--D (2) SATURN-IMPA WFC3/UVIS, ACCUM,
FQ727N
CR-SPLIT=NO
30 Secs (30 Secs)
CT-SITE
UVIS-QUAD-SUB
[==>]
[1]
Comments: EXPOSURE TIMES MUST BE REFINED !!
exposure time here is preliminary because target's heliocentric distance at time of observations is not known. once the timing of the impact is known, exposure times must be adjusted to maximize s/n ratio, avoid satura
tion, and optimize observational efficiency.
7
Orbit Structure
Proposal 13318 - SAT-2 (02) - Giant impacts on giant planets
8
Solar System Targets
Visit
Proposal 13318 - JUP-1 (03) - Giant impacts on giant planets
Proposal 13318, JUP-1 (03), implementation
Diagnostic Status: No Diagnostics
Scientific Instruments: WFC3/UVIS
Special Requirements: PCS MODE FINE; DROP TO GYRO IF NECESSARY NO REACQ; GYRO MODE 3GOBAD; SCHED 100%
Comments: jupiter visit #1 of 2
Thu Jul 11 18:55:22 GMT 2013
NOTE: Date of impact is unknown, so duration of visibilities cannot be predicted at this time. When observations are actually planned, we intend to duplicate or eliminate some exposures to fill the available visibility.
Current visit design is for 42-min visibility window.
#
Name
Level 1
Level 2
Level 3
Window
Ephem Center
(1)
JUPITER-IMPACT- STD=JUPITER
TYPE=PGRAPHIC,LONG=0,LAT=0
SEP OF JUPITER CALLISTO FROM EARTH
SITE
EARTH GT 50",
SEP OF JUPITER IO FROM EARTH
GT 50",
SEP OF JUPITER EUROPA FROM
EARTH GT 50",
SEP OF JUPITER GANYMEDE
FROM EARTH GT 50"
Comments: NEED TO REFINE LEVEL 2 COORDINATES AFTER IMPACT TAKES PLACE (or after impact location is predicted prior to impact)
9
Proposal 13318 - JUP-1 (03) - Giant impacts on giant planets
Exposures
#
1
Label
Target
Config,Mode,Aperture
FQ727N--D (1) JUPITER-IMPA WFC3/UVIS, ACCUM,
CT-SITE
UVIS-QUAD-SUB
Spectral Els.
FQ727N
Opt. Params.
CR-SPLIT=NO
Special Reqs.
Groups
Exp. Time (Total)/[Actual Dur.]
8 Secs (8 Secs)
[==>]
Orbit
[1]
Comments: EXPOSURE TIMES MUST BE REFINED !!
exposure time here is preliminary because target's heliocentric distance at time of observations is not known. once the timing of the impact is known, exposure times must be adjusted to maximize s/n ratio, avoid satura
tion, and optimize observational efficiency.
2
FQ889N--A (1) JUPITER-IMPA WFC3/UVIS, ACCUM,
FQ889N
CR-SPLIT=NO
60 Secs (60 Secs)
CT-SITE
UVIS-QUAD-SUB
[==>]
[1]
Comments: EXPOSURE TIMES MUST BE REFINED !!
exposure time here is preliminary because target's heliocentric distance at time of observations is not known. once the timing of the impact is known, exposure times must be adjusted to maximize s/n ratio, avoid satura
tion, and optimize observational efficiency.
3
F275W--A (1) JUPITER-IMPA WFC3/UVIS, ACCUM,
F275W
CR-SPLIT=NO
40 Secs (40 Secs)
CT-SITE
UVIS1-2K2A-SUB
[==>]
[1]
Comments: EXPOSURE TIMES MUST BE REFINED !!
exposure time here is preliminary because target's heliocentric distance at time of observations is not known. once the timing of the impact is known, exposure times must be adjusted to maximize s/n ratio, avoid satura
tion, and optimize observational efficiency.
4
F631N--A
(1) JUPITER-IMPA WFC3/UVIS, ACCUM,
F631N
CR-SPLIT=NO
4 Secs (4 Secs)
CT-SITE
UVIS1-2K2A-SUB
[==>]
[1]
Comments: EXPOSURE TIMES MUST BE REFINED !!
exposure time here is preliminary because target's heliocentric distance at time of observations is not known. once the timing of the impact is known, exposure times must be adjusted to maximize s/n ratio, avoid satura
tion, and optimize observational efficiency.
5
F502N--A
(1) JUPITER-IMPA WFC3/UVIS, ACCUM,
F502N
CR-SPLIT=NO
3.4 Secs (3.4 Secs)
CT-SITE
UVIS1-2K2A-SUB
[==>]
[1]
Comments: EXPOSURE TIMES MUST BE REFINED !!
exposure time here is preliminary because target's heliocentric distance at time of observations is not known. once the timing of the impact is known, exposure times must be adjusted to maximize s/n ratio, avoid satura
tion, and optimize observational efficiency.
6
F395N--A
(1) JUPITER-IMPA WFC3/UVIS, ACCUM,
F395N
CR-SPLIT=NO
9 Secs (9 Secs)
CT-SITE
UVIS1-2K2A-SUB
[==>]
[1]
Comments: EXPOSURE TIMES MUST BE REFINED !!
exposure time here is preliminary because target's heliocentric distance at time of observations is not known. once the timing of the impact is known, exposure times must be adjusted to maximize s/n ratio, avoid satura
tion, and optimize observational efficiency.
7
F225W--A (1) JUPITER-IMPA WFC3/UVIS, ACCUM,
F225W
CR-SPLIT=NO
150 Secs (150 Secs)
CT-SITE
UVIS1-2K2A-SUB
[==>]
[1]
Comments: EXPOSURE TIMES MUST BE REFINED !!
exposure time here is preliminary because target's heliocentric distance at time of observations is not known. once the timing of the impact is known, exposure times must be adjusted to maximize s/n ratio, avoid satura
tion, and optimize observational efficiency.
8
F343N--A
(1) JUPITER-IMPA WFC3/UVIS, ACCUM,
F343N
CR-SPLIT=NO
5.5 Secs (5.5 Secs)
CT-SITE
UVIS1-2K2A-SUB
[==>]
[1]
Comments: EXPOSURE TIMES MUST BE REFINED !!
exposure time here is preliminary because target's heliocentric distance at time of observations is not known. once the timing of the impact is known, exposure times must be adjusted to maximize s/n ratio, avoid satura
tion, and optimize observational efficiency.
9
FQ889N--A (1) JUPITER-IMPA WFC3/UVIS, ACCUM,
FQ889N
CR-SPLIT=NO
60 Secs (60 Secs)
CT-SITE
UVIS-QUAD-SUB
[==>]
[1]
Comments: EXPOSURE TIMES MUST BE REFINED !!
exposure time here is preliminary because target's heliocentric distance at time of observations is not known. once the timing of the impact is known, exposure times must be adjusted to maximize s/n ratio, avoid satura
tion, and optimize observational efficiency.
10
Orbit Structure
Proposal 13318 - JUP-1 (03) - Giant impacts on giant planets
11
Solar System Targets
Visit
Proposal 13318 - JUP-2 (04) - Giant impacts on giant planets
Proposal 13318, JUP-2 (04), implementation
Diagnostic Status: No Diagnostics
Scientific Instruments: WFC3/UVIS
Special Requirements: PCS MODE FINE; DROP TO GYRO IF NECESSARY NO REACQ; GYRO MODE 3GOBAD; SCHED 100%; AFTER 03 BY 5.9 Orbits TO 6.1 Orbits
Comments: jupiter visit #2 of 2
Thu Jul 11 18:55:23 GMT 2013
NOTE: Date of impact is unknown, so duration of visibilities cannot be predicted at this time. When observations are actually planned, we intend to duplicate or eliminate some exposures to fill the available visibility.
Current visit design is for 42-min visibility window.
#
Name
Level 1
Level 2
Level 3
Window
Ephem Center
(1)
JUPITER-IMPACT- STD=JUPITER
TYPE=PGRAPHIC,LONG=0,LAT=0
SEP OF JUPITER CALLISTO FROM EARTH
SITE
EARTH GT 50",
SEP OF JUPITER IO FROM EARTH
GT 50",
SEP OF JUPITER EUROPA FROM
EARTH GT 50",
SEP OF JUPITER GANYMEDE
FROM EARTH GT 50"
Comments: NEED TO REFINE LEVEL 2 COORDINATES AFTER IMPACT TAKES PLACE (or after impact location is predicted prior to impact)
12
Proposal 13318 - JUP-2 (04) - Giant impacts on giant planets
Exposures
#
1
Label
Target
Config,Mode,Aperture
FQ727N--D (1) JUPITER-IMPA WFC3/UVIS, ACCUM,
CT-SITE
UVIS-QUAD-SUB
Spectral Els.
FQ727N
Opt. Params.
CR-SPLIT=NO
Special Reqs.
Groups
Exp. Time (Total)/[Actual Dur.]
8 Secs (8 Secs)
[==>]
Orbit
[1]
Comments: EXPOSURE TIMES MUST BE REFINED !!
exposure time here is preliminary because target's heliocentric distance at time of observations is not known. once the timing of the impact is known, exposure times must be adjusted to maximize s/n ratio, avoid satura
tion, and optimize observational efficiency.
2
FQ889N--A (1) JUPITER-IMPA WFC3/UVIS, ACCUM,
FQ889N
CR-SPLIT=NO
60 Secs (60 Secs)
CT-SITE
UVIS-QUAD-SUB
[==>]
[1]
Comments: EXPOSURE TIMES MUST BE REFINED !!
exposure time here is preliminary because target's heliocentric distance at time of observations is not known. once the timing of the impact is known, exposure times must be adjusted to maximize s/n ratio, avoid satura
tion, and optimize observational efficiency.
3
F275W--A (1) JUPITER-IMPA WFC3/UVIS, ACCUM,
F275W
CR-SPLIT=NO
40 Secs (40 Secs)
CT-SITE
UVIS1-2K2A-SUB
[==>]
[1]
Comments: EXPOSURE TIMES MUST BE REFINED !!
exposure time here is preliminary because target's heliocentric distance at time of observations is not known. once the timing of the impact is known, exposure times must be adjusted to maximize s/n ratio, avoid satura
tion, and optimize observational efficiency.
4
F631N--A
(1) JUPITER-IMPA WFC3/UVIS, ACCUM,
F631N
CR-SPLIT=NO
4 Secs (4 Secs)
CT-SITE
UVIS1-2K2A-SUB
[==>]
[1]
Comments: EXPOSURE TIMES MUST BE REFINED !!
exposure time here is preliminary because target's heliocentric distance at time of observations is not known. once the timing of the impact is known, exposure times must be adjusted to maximize s/n ratio, avoid satura
tion, and optimize observational efficiency.
5
F502N--A
(1) JUPITER-IMPA WFC3/UVIS, ACCUM,
F502N
CR-SPLIT=NO
3.4 Secs (3.4 Secs)
CT-SITE
UVIS1-2K2A-SUB
[==>]
[1]
Comments: EXPOSURE TIMES MUST BE REFINED !!
exposure time here is preliminary because target's heliocentric distance at time of observations is not known. once the timing of the impact is known, exposure times must be adjusted to maximize s/n ratio, avoid satura
tion, and optimize observational efficiency.
6
F395N--A
(1) JUPITER-IMPA WFC3/UVIS, ACCUM,
F395N
CR-SPLIT=NO
9 Secs (9 Secs)
CT-SITE
UVIS1-2K2A-SUB
[==>]
[1]
Comments: EXPOSURE TIMES MUST BE REFINED !!
exposure time here is preliminary because target's heliocentric distance at time of observations is not known. once the timing of the impact is known, exposure times must be adjusted to maximize s/n ratio, avoid satura
tion, and optimize observational efficiency.
7
F225W--A (1) JUPITER-IMPA WFC3/UVIS, ACCUM,
F225W
CR-SPLIT=NO
150 Secs (150 Secs)
CT-SITE
UVIS1-2K2A-SUB
[==>]
[1]
Comments: EXPOSURE TIMES MUST BE REFINED !!
exposure time here is preliminary because target's heliocentric distance at time of observations is not known. once the timing of the impact is known, exposure times must be adjusted to maximize s/n ratio, avoid satura
tion, and optimize observational efficiency.
8
F343N--A
(1) JUPITER-IMPA WFC3/UVIS, ACCUM,
F343N
CR-SPLIT=NO
5.5 Secs (5.5 Secs)
CT-SITE
UVIS1-2K2A-SUB
[==>]
[1]
Comments: EXPOSURE TIMES MUST BE REFINED !!
exposure time here is preliminary because target's heliocentric distance at time of observations is not known. once the timing of the impact is known, exposure times must be adjusted to maximize s/n ratio, avoid satura
tion, and optimize observational efficiency.
9
FQ889N--A (1) JUPITER-IMPA WFC3/UVIS, ACCUM,
FQ889N
CR-SPLIT=NO
60 Secs (60 Secs)
CT-SITE
UVIS-QUAD-SUB
[==>]
[1]
Comments: EXPOSURE TIMES MUST BE REFINED !!
exposure time here is preliminary because target's heliocentric distance at time of observations is not known. once the timing of the impact is known, exposure times must be adjusted to maximize s/n ratio, avoid satura
tion, and optimize observational efficiency.
13
Orbit Structure
Proposal 13318 - JUP-2 (04) - Giant impacts on giant planets
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