FM172

Looking at the Restart states from Rev 173 we have the following results for FM172.

FM139	 	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 (m)	 	
MMS1	Sep 01 2015 16:54:26.522	42108.529	42099.326	42099.330	-9.203	-9.199	-4.091	0.04%	
MMS2	Sep 01 2015 16:55:12.146	42108.514	42112.084	42112.095	3.570	3.581	-10.922	-0.31%	
MMS3	Sep 01 2015 16:55:45.459	42108.483	42101.593	42101.627	-6.890	-6.855	-34.699	0.50%	
MMS4	Sep 01 2015 16:56:21.824	42108.622	42108.622	42108.631	0.000	0.009	-8.928		

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.
The predicted velocity meets all requirements with significant margin.
Maneuver ID	Timespan	DVX (m/s)/ 
Req. (m/s)/
DiffVX(m/s)	DVY (m/s)/
Req. (m/s)/
DiffVY(m/s)	DVZ (m/s)/
Reg. (m/s)/
DiffVZ(m/s)	
MMS1_FM172	243/19:15:35 – 243/19:17:35	-0.831106	-1.033227	0.269147	
		0.010	0.010	0.010	
		0.00005	0.0003	0.0001	
MMS2_FM172	244/00:25:35 - 244/00:26:55	0.836966	-0.354026	-0.437572	
		0.010	0.010	0.010	
		0.0005	0.0015	0.0005	
MMS3_FM172	244/01:55:35 - 244/02:01:55	-1.410087	-0.409801	2.079666	
		0.014	0.010	0.020	
		0.0005	0.003	0.0015