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Mnemonic:

3GM_GRAVITY_FOR_EPHEMERIDES

Name:

3GM GRAVITY FOR EPHEMERIDES

Description:

KaT ON during communication windows

Payload:

3GM

Pointing

Pointing Type:

none

Target:

PTRSnippet file:

Advanced

Scheduling Rules:

during station visibility. 3GM_HAA_STANDBY should start at least 48 hours before 3GM_GRAVITY_FOR_EPHEMERIDES starts if not already scheduled in parallel
This observation should be preceded by 3GM_HAA_CALIBRATION

any rule that is used to schedule the observation: repetition rules, continuous (plasma instruments), one-off, every orbit, every day, etc

Avoidance Rules:

TBD

conditions that make the observation not possible (e.g. thruster firing)

Comments:

#update2020

Support Plot 1:

Support Plot 2:

Support Plot 3:

Commanding

ITLSnippet file:

Related segment definitions

	Segmentdefinition
Segment	E_distant
Segment	E_IS
Segment	G_distant
Segment	CAL
Segment	DL_
Segment	DL_EXT
Segment	G_IS_OBS
Segment	C_IS_OBS
Segment	E_IS_OBS
Segment	C_distant

Power profiles

	Event	Time	Mode	User Defined Power (Watts)	Comment
Start 00:00:00 User Defined 35.14 [Watt]	Start	00:00:00	User Defined	35.14	only KaT power accounted for, as HAA is already ON (3GM_HAA_STANDBY observation) there is no additional HAA power to be accounted for (just a change in HAA mode from STANDBY to OBSERVATION mode, with no impact on power) JUI-3GM-INST-UM-001, v1.2

Data profiles

	Event	Time	Mode	User Defined Data Rate (bit/s)	Comment
Start 00:00:00 User Defined 1543.2 [bit/s]	Start	00:00:00	User Defined	1543.2	HAA in nominal science (HAA from STANDBY to CALIBRATION and OBSERVATION mode) JUI-3GM-INST-UM-001, v1.2

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