FM435

Looking at the Restart states from Rev 435 we have the following results for FM435.
FM435		NoBurn	Plan	OD	Plan-NoBurn	OD-NoBurn	Plan-OD	SMA error	
MMS	Epoch of Plan Apogee	A(km)	A (km)	A (km)	A (km)	A (km)	A (km)		
MMS1	May 20 2016 10:56:10.534	42101.672	42107.225	42107.238	5.55264	5.56521	-0.01258	-0.23%	
MMS3	May 20 2016 10:55:38.234	42103.490	42107.213	42107.219	3.72311	3.72945	-0.00634	-0.17%	
MMS4	May 20 2016 10:55:44.452	42105.148	42107.220	42107.218	2.07184	2.06928	0.00256	0.12%	

All three DVs were more radial this time.
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)	
MMS1_FM435	2016_140/08:03:46 to 2016_140/08:04:36	0.1267	-0.5725	-0.1927	
		0.002	0.005725	0.002	
		-0.0004263	-0.0004394	-0.0003546	
MMS3_FM435	2016_140/09:38:46 to 2016_140/09:39:36	0.1277	-0.6335	-0.087	
		0.002	0.006335	0.002	
		-0.0006403	-0.001038	-0.0006063	
MMS4_FM435	2016_140/11:13:56 to 2016_140/11:14:36	0.2036	-0.4393	-0.2064	
		0.002036	0.004393	0.002064	
		-0.0007855	-0.001752	-0.0009799