FR307

Looking at the Restart states from Rev 308 we have the following results for FR307.

FR307		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 14 2016 01:55:33.956	42102.228	42105.255	42105.302	3.027	3.074	-0.04727	-1.56%	
MMS2	Jan 14 2016 01:55:57.878	42102.184	42108.255	42108.318	6.071	6.134	-0.06324	-1.04%	
MMS3	Jan 14 2016 01:55:27.565	42102.212	42102.212	42102.272	0.000	0.060	-0.06026		
MMS4	Jan 14 2016 01:55:28.863	42102.177	42100.906	42100.938	-1.270	-1.238	-0.03212	2.53%	

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

FR307	Plan Change Plan	Plan Change OD	error	
MMS4	0.05995	0.05996	0.017%	

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_FR307	013/10:05:15-013/10:09:45	-0.86591	0.83866	-0.35979	
		0.01	0.01	0.01	
		0.0015	0.0022	0.0015	
MMS2_FR307	013/06:35:15-013/06:39:45	0.047606	0.9891	-0.30039	
		0.01	0.01	0.01	
		0.0002	0.0006	0.0007	
MMS4_FR307	013/08:00:15-013/08:06:25	-0.051999	0.56669	-1.1144	
		0.01	0.01	0.011144	
		0.0001	0.0006	0.0007