FR1347

Looking at the Restart states from Rev 1348 we have the following results for FR1347
FR1347		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	Aug 31 2022 04:18:58	97773.259	97764.320	97764.318	-8.939	-8.941	0.002	-0.019%	-0.242%	
MMS2	Aug 31 2022 04:19:12	97773.467	97773.467	97773.485	0.000	0.019	-0.019			
MMS3	Aug 31 2022 04:19:15	97773.414	97780.414	97780.405	7.001	6.991	0.010	0.136%	0.290%	
MMS4	Aug 31 2022 04:19:55	97773.419	97785.238	97785.258	11.819	11.839	-0.020	-0.168%	0.109%	
 
MMS1 was 0.2805 m/s (net delta-v) and 58% axial, MMS3 was 0.3276 m/s and 42.50% axial, and MMS4 was 0.2688 m/s and 42.16% 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_FR1347	2022_240/17:36:12 to 2022_240/17:36:42		-0.1904	0.1487	-0.1142	
		0.01	0.01	0.01	
		-0.002849	-0.0008055	-0.008503	
MMS3_FR1347	2022_240/19:11:12 to 2022_240/19:11:52		0.1149	0.1474	0.2711	
		0.01	0.01	0.01	
		-0.006503	-0.002233	-0.006287	
MMS1_FR1347	2022_240/20:46:12 to 2022_240/20:47:02
		0.1508	0.1437	-0.1847	
		0.01	0.01	0.01	
		-0.002902	-0.001905	-0.003232