AR703

Looking at the Restart states from Rev 704 we have the following results for AR703.
AR703		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)			
MMS2	Feb 12 2017 07:35:13.649	42109.436	44916.363	44917.280	2806.928	2807.844	-0.91601	-0.03%	1.46%	
		Period (min)	Period (min)	Period (min)	Period (min)	Per. (min)	Per. (min)	P-OD Per. (secs)		
MMS2	Feb 12 2017 07:34:39.561	1433.273	1578.944	1578.992	145.671	145.719	-0.04830	-2.90		
 
MMS2 was 31.24 m/s using 21.097 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 MMS2 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)	
MMS2_AR703	2017_41/15:41:59.711 to 2017_41/16:32:49.711	-30.2058	-7.7222	-2.2324	
		0.302058	0.077222	0.022324	
		0.01	-0.006	0.009