FR308

Looking at the Restart states from Rev 309 we have the following results for FR308.

FR308		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	Jan 15 2016 01:48:31.189	42105.562	42102.517	42102.527	-3.045	-3.036	-0.00977	0.32%	
MMS2	Jan 15 2016 01:48:35.917	42108.580	42102.538	42102.547	-6.041	-6.033	-0.00854	0.14%	
MMS3	Jan 15 2016 01:48:22.446			42102.527					
MMS4	Jan 15 2016 01:48:31.021	42101.198	42102.501	42102.514	1.303	1.317	-0.01348	-1.03%	

MMS4 is more of a plane change maneuver and the results relative to that are the following:

FR308	Plan Change Plan	Plan Change OD	error	
MMS4	0.043349	0.043476	0.292%	

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_FR308	014/02:47:10-014/02:51:00	-0.35535	-0.25561	0.42619	
		0.0035535	0.0025561	0.0042619	
		-0.0014	-0.0025	0.0011	
MMS2_FR308	013/23:36:40-013/23:41:00	0.056265	0.4783	0.97064	
		0.002	0.004783	0.0097064	
		-0.0008	-0.001	-0.0005	
MMS4_FR308	014/01:11:30-014/01:16:00	-0.060257	-0.7183	0.45323	
		0.002	0.007183	0.0045323	
		-0.001	-0.0015	-0.0005