FR378

Looking at the Restart states from Rev 379 we have the following results for FR378.

FR378		NoBurn	Plan	OD	Plan-NoBurn	OD-NoBurn	Plan-OD	error	
MMS	Epoch of Plan Apogee	A(km)	A (km)	A (km)	A (km)	A (km)	A (km)		
MMS1	Mar 24 2016 17:30:44.698	42101.233	42097.569	42097.576	-3.66418	-3.65686	-0.00731	0.20%	
MMS2	Mar 24 2016 17:30:47.058	42101.222	42104.110	42104.131	2.88847	2.90940	-0.02093	-0.72%	
MMS3	Mar 24 2016 17:30:39.042	42101.238	42103.482	42103.500	2.24425	2.26278	-0.01853	-0.83%	
MMS4	Mar 24 2016 17:30:41.057	42101.234	42101.234	42101.254	0.00000	0.01952	-0.01953		

All three DVs were highly axial and had plan change errors of 0.28%, 0.30% and 0.16% respectively.
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 planning 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 maneuvering spacecraft meet 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_FR378	2016_83/21:36:11 to 2016_83/21:38:01	0.1815	0.4017	-0.4814	
		0.01	0.01	0.01	
		0.0005	0.0007	0.00075	
MMS1_FR378	2016_83/23:11:11 to 2016_83/23:12:51	0.0209	-0.0042	-0.6186	
		0.01	0.01	0.01	
		0.0006	0.00175	0.00125	
MMS2_FR378	2016_84/00:46:11 to 2016_84/00:48:01	-0.1061	0.5104	-0.4306	
		0.01	0.01	0.01	
		-0.00025	0.0035	0.002