No prob, I just needed that clarification.
I can see what the problem is and why TransX doesn't come up with the same result as IMFD, when you use the Auto-min. The Outward velocity is 'maxed out' at 1000 m/s and can't go beyond that in order to get you to the trajectory needed for the arrival date of MAVEN's actual filght.
You see the Auto-Min feature needs to have some constraints in order to arrive at sensible
optimal trajectories. Those are +/- 4.5 km/s for the Pl.Change and +/- 1 km/s for the Outward velocity. (and I think +/- 50% of the hohmann transfer at the time of the scenario start for the Prograde vel.)
I have already proposed to Enjo to give a little more "room" at the Outward velocity constraint, but it seems that this creates more problems than it solves.
IMFD doesn't have that problem because the user enters the Departure
and Arrival dates and the Lambert solver finds the solution for those two variables, while TransX's Auto-Min doesn't have an arrival date variable.
Another thing to watch is that Maven's heliocentric transfer is not exactly optimal, with the heliocentric transfer Delta-V at ~3.48 km/s.
Enjo might be able to clarify a bit more on this, for now I can leave you with the TransX plan tweaked for an arrival ~ at the actual arrival date. It will need more tweaking to match the parking orbit.
Code:
BEGIN_DESC
Contains the latest simulation state.
END_DESC
BEGIN_ENVIRONMENT
System Sol
Date MJD 56614.7943659233
END_ENVIRONMENT
BEGIN_FOCUS
Ship GL-01
END_FOCUS
BEGIN_CAMERA
TARGET GL-01
MODE Cockpit
FOV 40.00
END_CAMERA
BEGIN_HUD
TYPE Surface
END_HUD
BEGIN_MFD Left
TYPE User
MODE TransX
Ship GL-01
FNumber 3
Int 1
Orbit True
Vector 5818633.35266 -2897680.34591 853485.385605
Vector -3227.38346184 -4995.36169662 5042.71940807
Double 3.98600439969e+014
Double 56614.7943654
Handle Earth
Handle NULL
Handle NULL
Select Target
0 Escape
Autoplan
0 0
Plan type
0 0
Plan
0 1
Plan
0 0
Plan
0 0
Select Minor
0 None
Manoeuvre mode
0 0
Auto-Center™
0 0
Base Orbit
0 0
Prograde vel.
1 0
Man. date
1 56614.7943651
Outward vel.
1 0
Ch. plane vel.
1 0
Intercept with
0 0
Orbits to Icept
0 0
Graph projection
0 0
Scale to view
0 0
Advanced
0 0
Pe Distance
1 6566000
Ej Orientation
2 -0.959232956896
Equatorial view
0 0
Finvars
Finish BaseFunction
Int 2
Orbit False
Handle Sun
Handle Earth
Handle Mars
Select Target
0 Mars
Autoplan
0 0
Plan type
0 2
Plan
0 0
Plan
0 0
Plan
0 1
Select Minor
0 None
Manoeuvre mode
0 0
Auto-Center™
0 0
Base Orbit
0 1
Prograde vel.
1 0
Man. date
1 56614.7943651
Outward vel.
1 0
Ch. plane vel.
1 0
Intercept with
0 0
Orbits to Icept
0 0
Graph projection
0 0
Scale to view
0 0
Advanced
0 0
Prograde vel.
5 2326.86086678
Eject date
9 56614.7918959
Outward vel.
4 -2299.29298742
Ch. plane vel.
3 -1147.12999532
Finvars
Finish BaseFunction
Int 5
Orbit True
Vector 6109590907.08 110158854.411 1419862954.74
Vector -3102.21729463 -54.1646594957 -721.957421058
Double 4.28282991638e+013
Double 56899.7970238
Handle Mars
Handle NULL
Handle NULL
Select Target
0 None
Autoplan
0 0
Plan type
0 1
Plan
0 0
Plan
0 2
Plan
0 0
Select Minor
0 None
Manoeuvre mode
0 0
Auto-Center™
0 0
Base Orbit
0 0
Prograde vel.
1 0
Man. date
1 56614.7785952
Outward vel.
1 0
Ch. plane vel.
1 0
Intercept with
0 0
Orbits to Icept
0 0
Graph projection
0 0
Scale to view
0 0
Advanced
0 0
Draw Base
0 0
Finvars
Finish BaseFunction
END_MFD
BEGIN_MFD Right
TYPE User
MODE TransX
END_MFD
BEGIN_SHIPS
GL-01:DeltaGlider
STATUS Orbiting Earth
RPOS 5818499.69 -2897887.22 853694.23
RVEL -3227.724 -4995.192 5042.669
AROT -66.15 -49.30 110.16
AFCMODE 7
PRPLEVEL 0:1.000000 1:1.000000
NAVFREQ 0 0 0 0
XPDR 0
AAP 0:0 0:0 0:0
END
END_SHIPS
BEGIN_ExtMFD
END
The parking orbit is ~12° off-plane with the hypothetical trajectory, but I have adjusted the Ej. Orientation, so that the node and the periapsis coincide. So it will take only one periapsis "kick" to raise the apoapsis, take care of the Rinc there, and finish the burn on the return back to periapsis.
Hope this helped.