AR704

Looking at the Restart states from Rev 705 we have the following results for AR704.
AR704		NoBurn	Plan	OD	Plan-NoBurn	OD-NoBurn	Plan-OD	SMA error	PC error	
MMS	Epoch of Plan Apogee	A(km)	A (km)	A (km)	A (km)	A (km)	A (km)			
MMS3	Feb 13 2017 07:28:12.364	42109.038	44915.068	44915.719	2806.030	2806.681	-0.65108	-0.02%	0.11%	
		Period (min)	Period (min)	Period (min)	Period (min)	Per. (min)	Per. (min)	P-OD Per. (secs)		
MMS3	Feb 13 2017 07:28:12.364	1433.252	1578.875	1578.910	145.623	145.657	-0.03433	-2.06		
 
MMS3 was 31.24 m/s using 20.99 kg
The Table below provides the following information:
•	First row for each maneuver: planned maneuver total delta-V values based on the associated DVTABLEs  
•	Second row for each maneuver: associated final maneuver p lanning requirements 
•	Third row for each maneuver: predicted velocity error at the time of the maneuver computed by differencing the predicted velocity at the maneuver time (starting with the post-perigee GEONS state prior to the maneuver) vs the definitive GEONS state at the time of the maneuver.
As shown in the table below, all MMS3 meets the requirement.
Maneuver ID	Timespan	DVX (m/s)/ 
Req. (m/s)/
DiffVX(m/s)	DVY (m/s)/
Req. (m/s)/
DiffVY(m/s)	DVZ (m/s)/
Req. (m/s)/
DiffVZ(m/s)	
MMS3_AR704	2017_42/15:35:07.526 to 2017_42/16:25:47.526	-30.186	-7.737	-2.2995	
		0.30186	0.07737	0.022995	
		0.015	0.005	0.006