AR712

Looking at the Restart states from Rev 714 we have the following results for AR712.
AR712		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)			
MMS4	Feb 22 2017 19:19:07.006	47455.686	51108.375	51109.701	3652.689	3654.015	-1.32592	-0.04%	0.08%	
		Period (min)	Period (min)	Period (min)	Period (min)	Per. (min)	Per. (min)	P-OD Per. (secs)		
MMS4	Feb 22 2017 19:19:07.006	1714.716	1916.452	1916.526	201.736	201.810	-0.07458	-4.47		
 
MMS4 was 31.80 m/s using 20.65 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, MMS4 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)	
MMS4_AR712	2017_51/18:58:39.065 to 2017_51/19:50:49.065	-30.6415	-8.2541	-2.013	
		0.306415	0.082541	0.02013	
		-0.009724	0.008573	0.001594