FM1452

Looking at the Restart states from Rev 1454 we have the following results for FM1452
FM1452		NoBurn	Plan	OD	Plan-NoBurn	OD-NoBurn	Plan-OD	SMA error	PC error	
MMS	Epoch of Plan Apogee	A(km)	A (km)	A (km)	A (km)	A (km)	A (km)			
MMS1	Sep 06 2023 17:59:60	97321.285	97321.258	97321.216	-0.027	-0.069	0.042	 		
MMS2	Sep 06 2023 18:00:24	97211.247	97321.125	97320.997	109.878	109.750	0.128	0.117%	-1.138%	
MMS3	Sep 06 2023 18:00:36	97168.210	97321.233	97321.117	153.023	152.907	0.117	0.076%	-0.399%	
MMS4	Sep 06 2023 18:00:27	97236.402	97321.126	97321.027	84.725	84.625	0.100	0.118%	-0.109%	
 
MMS2 was 2.0612 m/s (net delta-v) and 24.91% axial, MMS3 was 2.4087 m/s and 31.89% axial, and MMS4 was 1.1782 m/s and 22.09% axial.
The Table below provides the following information:
•	The start and end times and planned maneuver 
•	Total delta-V (DeltaV_X, DeltaV_Y, and DeltaV_Z) for the first maneuver extracted from the DVTABLE files, 
•	The associated predicted velocity maneuver planning requirement for 1 and 2 orbit predictions (DeltaV_X Req, DeltaV_Y Req, and DeltaV_Z Req)
•	The difference between the predicted velocity and the GEONS definitive velocity at the start time of the first maneuver (Diff_V_X, Diff_V_Y, and Diff_V_Z).Planned maneuver total delta-V values based on the associated DVTABLEs    
As shown in the table below, all 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)	
MMS4_FM1452	2023_241/11:37:47 to 2023_241/11:39:37		0.8557	-0.6323	-0.5089	
		0.008557	0.006323	0.005089	
		0.006312	0.002417	0.0009749	
MMS3_FM1452	2023_241/13:26:07 to 2023_241/13:29:37	1.5997	-1.1902	-1.352	
		0.015997	0.011902	0.01352	
		0.005258	0.001647	-0.006377	
MMS2_FM1452	2023_241/15:16:27 to 2023_241/15:19:37	1.296	-1.2237	-1.0327	
		0.01296	0.012237	0.010327	
		0.00346	0.001789	0.0008027