1. Current SOC-Ground System Integration Schedule (Jan 18-19 2007)
2006
2007
2008 D J F M A M J J A S O N D J F M A M J J A S O
Ground System Reviews
Mission Operation review
September (TBC)
SOC Telemetry and Command (T&C)
EVE/MOC Integration
Jun Jan
HMI/MOC Integration
Feb Mar
AIA/MOC Integration
Mar Apr
All SOCs/MOC Integration.
Apr Apr
SOC Science Data Processing (SDP)
EVE/DDS Preliminary
Feb Mar
EVE/DDS Integration
Apr - May 2007
Depends on DDS 60-day test
HMI/DDS Integration
Jul Aug
AIA/DDS Integration
Aug Sep
All SOCs/MOC Integ.
Sep Sep
Communications lines
EVE/MOC T1 (1)
Done: June
HMI-AIA/MOC T1
Jan 2007
Pending
EVE/DDS T3
April 2007
May be revised
HMI/DDS OC3
July
Request Jan 25
AIA/DDS OC3
Aug
Request Feb 26
GSRT#4b 72-day end-to-end performance test
Oct/Dec 2007 1

2. Mission Ops Test Milestones with Observatory
2007
2008
Nov
Jan
Mar
May
Jul
Sept
Nov
Jan
Mar
May
July
Sept
Observatory Integration and Testing
PSR
Launch
Aug 08
Mission Operations Reviews
MOR
FORR
1st SDO H/K Data Flow with MOC
(S/C only)
(AIA, EVE, HMI)
FOT Flight Procedure Testing with Spacecraft
(TV/TB)
High-rate OC3 Data Circuit S/C I&T to WSC
MOC Contingency Procedure Testing with Instruments
Mission Simulations
(ETE, and Day in Life)
Mission Simulations During TV/TB Testing
Mission Simulations Contingency Operations
Mission Simulations L&EO Operations
Testing with SDO at KSC
Launch Rehearsals
Last Revision: January 2007 1

3. Test Opportunities w/ Observatory (1 of 3)
Test Opportunity
Date
~ Test Hours
Comments
First Spacecraft Housekeeping Dataflow with MOC
March 2007 24
First live telemetry data transmitted to MOC from the spacecraft.
Testing will include No-Op commanding to verify command coordination between MOC and I&T T&C systems
Performed after C&DH electrical integration is complete
Once interface is established, telemetry can be flowed to the MOC on an as needed basis (coordinated with S/C TCs)
Telemetry can also be sent to SOCs as needed (to be negotiated between Instrument Teams and FOT)
MOC Flight Procedure Testing with Spacecraft
June
2007 48
FOT requires time with spacecraft to test contingency procedures that cannot be tested with the FlatSat simulator. (For example cross-strapping procedures)
Time may be spread out over several days, executed during off-hours
First EVE Housekeeping Dataflow to EVE SOC
Aug 2007
First live EVE instrument housekeeping telemetry data transmitted through the MOC to the EVE SOC
Performed after EVE instrument integration is complete
EVE housekeeping telemetry can be sent to SOC (via MOC) on an as needed basis (to be negotiated between EVE Team and FOT)
First HMI Housekeeping Dataflow to JSOC
First live HMI instrument housekeeping telemetry data transmitted through the MOC to the JSOC
Performed after HMI instrument integration is complete
HMI housekeeping telemetry can be sent to JSOC (via MOC) on an as needed basis (to be negotiated between HMI Team and FOT)
First AIA Housekeeping Dataflow to JSOC
First live AIA instrument housekeeping telemetry data transmitted through the MOC to the JSOC (performed after AIA instrument integration is complete)
AIA housekeeping telemetry can be sent to JSOC (via MOC) on an as needed basis (to be negotiated between AIA Team and FOT) 1

4. Test Opportunities w/ Observatory (2 of 3)
Test Opportunity
Date
~ Test Hours
Comments
MOC Flight Procedure Testing with Instruments
Jan 2008 48
This time is reserved for the FOT and SOCs to jointly test and validate Instrument contingency procedures which reside in the MOC (for example instrument safing or shutdown)
Time may be spread out over several days and executed during off-hours
MOC/SOC Ka-band
End-to-End (ETE) Dataflow Test
Feb 2008 24
This simulation will focus on High-rate science data from the Instruments over a temporary OC3 circuit from GSFC to WSC through the operational DDS and to the SOC SDP facilities
Project plans to install GSFC-to-WSC OC3 circuit for approx 90 days to support this testing (currently planned for Jan through March 2008)
Day in The Life
Mission Simulation
Simulate typical SDO day in the life (Full sun ops)
This simulation will include High-rate science data from the Instruments over the temporary OC3 circuit from GSFC to WSC
Mission Planning Meeting (discuss planned MOC and SOC activities)
Will include SOC-MOC command link coordination
SOC uplink of routine command loads
FOT uplink of ATS and EPV loads, automated SSR retransmissions, etc.
Mission Simulations During TV/TB
Feb-Apr 2008 84
Simulate typical SDO day in the life (Full-sun and Eclipse ops)
These simulations will focus on the planning and coordination between the MOC and SOCs specific to Eclipse Operations.
Simulations will likely be executed piecemeal as several separate opportunities scheduled around thermal transition periods
OC3 circuit should still be in place allowing flow of High-rate science telemetry to be included in simulations 1

5. Test Opportunities w/ Observatory (3 of 3)
Test Opportunity
Date
~ Test Hours
Comments
Mission Simulation
Contingency Operations
April 2008 48
Contingency Tests and Simulations: This time is set aside for simulating/testing the MOC’s ability to handle various contingency scenarios that cannot be simulated with the FlatSat
Examples include: C&DH, ACE, and GCE Cross-strap configurations, HGA Handovers, Loss of Comm recovery, and Ka-band and S-band RF configurations, Instrument Contingencies (TBD)
Mission Simulations
L&EO Simulations
Apr-May 2008 24
L&EO Simulations: Time is set aside for the MOC and SOCs to test and simulate planned IOC activities which cannot be simulated with the FlatSat
Examples include Instrument Turn On and Initialization activities using IGSE located in the MOC SOS.
Launch Rehearsals
(Three total)
Jul-Aug 2008
24 hours
Rehearse the timeframe from Launch minus 8-hours to Launch
All mission support personnel participate in these rehearsals to assure that all channels of communication have been well thought out and exercised 1