AXAF Standard Operating Procedure |
DATE: 07/19/99 REV: 3.1
SOP_61036_DEAA_ON.doc |
PROCEDURE: deaa_on.ps rev 2.0
61036.1 OVERVIEW
This is an "atomic" procedure which simply powers on the DEA side A .
61036.2 SUPPORT SUMMARY
SUMMARY |
Enable and turn on DEA power supply side A |
CONSTRAINTS |
Requires FMT 1,2,4, or 6 DEA B must be off |
INITIAL CONDITIONS |
Assumes that the PSMC has power from the spacecraft |
Author: A. Northrup |
EST. Time : 00:03
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AXAF Standard Operating Procedure |
DATE: 07/19/99 REV: 3.1
SOP_61036_DEAA_ON.doc |
DISPLAYS |
F_OPERATIONS_COMMAND I_ACIS_E_NEW |
COMPS | None |
COMMAND GROUPS | None |
PIX MAPS | None |
COMMAND LOADS | None |
SCRIPTS | I_1_DEAA_ON |
A. Set the following command system configuration parameters:
Clear To Send Mechanism | = FSV |
CAR Processing | = Enabled |
FSV Processing | = Enabled |
CRR Processing | = Disabled |
Output Format | = NRZM |
Minimum Time Delay (sec) | = 3 |
CAR Time-out (sec) | = 40 |
FSV Time-out (sec) | = 45 |
Blocking Factor | = 90 |
Burst Factor | = 1 |
A. SOT authorizes OC to start script I_1_DEAA_ON.
B. OC may resume past initial wait.
Script uplinks command
1DEPSAEN {1.1}
Script uplinks command
1DEPSAON {1.2}
[DEA A ON]
C. OC informs SOT that script has completed.
D. Verify telemetry .
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DEA A Enable |
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DEA A On |
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DEA Input V A |
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DEA Input I A |
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DEA +24 V A |
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DEA +6 V A |
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DEA -6 V A |
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DEA +15 V A |
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DEA -15 V A |
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DEA +28 V A |
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DEA Input I B |
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DEA +24 V B |
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DEA +6 V B |
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DEA -6 V B |
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DEA +15 V B |
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DEA -15 V B |
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DEA +28 V B |
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END OF PROCEDURE
Author: A. Northrup |
EST. Time : 00:03
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