OK. So i figured a hohmann transfer to the moon at a time that allowed a Pe sitting at the axis (node) with the ship orbiting the moon would be a good start. Then an orbit insert but with high Ap and single plane change at Ap then usual rendezvous.
I set up a ship on the Earth and flew it into LEO in plane with the moon. The trick was when to leave to arrive with the Pe at a node.
I first placed myself in the shuttle around the moon and made a TransX plan for return to Earth with just negative prograde and no plane change or inward. I adjusted eject orientation and date of plan to find where the shuttle is already in plane with the plan. I figured if I could leave the moon at that time from that orbit and fall to Earth in plane with the moon then I should be able to do the reverse. Time knows no direction right? LOL It showed 61265.3
Then I glanced at IMFD Map and saw what the axis of the shuttle is and it appeared that somewhere about 61263 to 61265 give or take a couple days should be a good time to leave or arrive at the moon from the shuttle's orbit.
So I tweaked a maneuver to transfer to the moon and it turned out that I was near the end of a window. I didn't want to wait 14 days so I accepted it as is.
Here's the scenario of the ship ready to eject to the moon. I flew it and found that a MCC a day or two before arriving moon allowed a tiny 15 m/s burn to shift the node directly onto the Pe. After the first orbit insert the high Ap had a single 75 m/s plane change.
Code:
BEGIN_DESC
Orbiter saved state at T = 690
END_DESC
BEGIN_ENVIRONMENT
System Sol
Date MJD 61258.7718168139
END_ENVIRONMENT
BEGIN_FOCUS
Ship GL-01
END_FOCUS
BEGIN_CAMERA
TARGET GL-01
MODE Cockpit
FOV 50.19
END_CAMERA
BEGIN_HUD
TYPE Orbit
REF AUTO
END_HUD
BEGIN_MFD Left
TYPE User
MODE TransX
Ship GL-01
FNumber 2
Int 0
Orbit True
Vector -540983.296661 494276.573149 6544013.187
Vector -7743.73281431 -409.118766793 -598.828496664
Double 3.98600439969e+014
Double 61258.727397
Handle Earth
Handle NULL
Handle Moon
Select Target
0 Moon
Autoplan
0 0
Plan type
0 0
Plan
0 0
Plan
0 0
Plan
0 0
Select Minor
0 None
Manoeuvre mode
0 1
Base Orbit
0 0
Prograde vel.
3 3124.23058924
Man. date
5 61258.8238519
Outward vel.
0 0
Ch. plane vel.
6 0
Intercept with
0 0
Orbits to Icept
0 0
Graph projection
0 0
Scale to view
0 0
Advanced
0 0
Finvars
Finish BaseFunction
Int 0
Orbit True
Vector -315937521.994 -29468897.1113 -185372582.952
Vector 753.507674961 71.4192780185 456.412786902
Double 4.90279493298e+012
Double 61258.5023002
Handle Moon
Handle NULL
Handle SA-1
Select Target
0 SA-1
Autoplan
0 0
Plan type
0 1
Plan
0 0
Plan
0 -1
Plan
0 0
Select Minor
0 None
Manoeuvre mode
0 0
Base Orbit
0 0
Prograde vel.
0 0
Man. date
0 61258.7718155
Outward vel.
0 0
Ch. plane vel.
0 0
Intercept with
0 0
Orbits to Icept
0 0
Graph projection
0 0
Scale to view
0 0
Advanced
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 6535763.12 255134.58 -630313.94
RVEL 723.931 647.751 7733.256
AROT 6.19 -1.33 -3.70
VROT 0.00 0.07 0.00
RCSMODE 2
AFCMODE 7
PRPLEVEL 0:0.579274 1:0.989132
NAVFREQ 402 94 0 0
XPDR 0
TRIM 1.000000
AAP 0:0 0:0 0:0
END
SA-1:ShuttleA
STATUS Orbiting Moon
RPOS -756214.65 457531.33 -1624128.83
RVEL -759.919 -1437.609 -60.095
AROT -132.76 38.02 94.70
AFCMODE 7
PRPLEVEL 0:0.857008 1:0.989253
NAVFREQ 0 0
XPDR 0
PODANGLE 3.1416 3.1416
DOCKSTATE 0 0.0000
AIRLOCK 0 0.0000
GEAR 1 1.0000
PAYLOAD MASS 0.0 0
END
END_SHIPS
BEGIN_VistaBoost
END