AR715

Looking at the Restart states from Rev 716 we have the following results for AR715.
AR715		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 26 2017 09:12:24.811	47451.023	51100.237	51101.100	3649.214	3650.077	-0.86246	-0.02%	0.12%	
		Period (min)	Period (min)	Period (min)	Period (min)	Per. (min)	Per. (min)	P-OD Per. (secs)		
MMS3	Feb 26 2017 09:12:24.811	1714.463	1915.994	1916.042	201.531	201.579	-0.04851	-2.91		
 
MMS3 was 31.73 m/s using 20.69 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, MMS3 meets the requirement except with VZ slightly over.
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_AR715	2017_55/08:52:8.791 to 2017_55/09:45:38.791	-30.5459	-8.3362	-2.0815	
		0.305459	0.083362	0.020815	
		-0.03601	-0.01889	-0.02135