I don't have the AMSO loaded but thought I would play with trajectories to see if a tour could be done with less encounter speed back at Earth. Found a tour of EVEEJSE with final Earth encounter speed of around 13.3 km/s. The TransX plan is in this deltaglider scenario set up a couple of minutes before the Apollo 16 launch. Haven't flown it but it looks fairly straightforward.
[edit] Noticed that in moving the launch time to actual time the date of eject was a bit off. I repaired this error and cleaned up the initial eject values with cleanup also of all slings. The repaired scenario is below the first one.
Code:
BEGIN_DESC
Trajectory for imaginary Apollo 16 mutiny to fly to Venus Earth Earth Jupiter Saturn Earth with encounter speed at Earth of between 13 and 14 Km/s.
END_DESC
BEGIN_ENVIRONMENT
System Sol
Date MJD 41423.6608966608
END_ENVIRONMENT
BEGIN_FOCUS
Ship 3
END_FOCUS
BEGIN_CAMERA
TARGET 3
MODE Cockpit
FOV 60.00
END_CAMERA
BEGIN_MFD Left
TYPE User
MODE TransX
Ship 3
FNumber 13
Int 1
Orbit True
Vector 5585148.10197 2716663.56664 1419739.73385
Vector -16.1872997656 -162.279300156 374.200084881
Double 3.98600439969e+014
Double 41423.660896
Handle Earth
Handle NULL
Handle NULL
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Plan
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Plan
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Plan
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Select Minor
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Manoeuvre mode
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Base Orbit
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Prograde vel.
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Man. date
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Outward vel.
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Ch. plane vel.
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Intercept with
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Orbits to Icept
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Graph projection
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Scale to view
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Advanced
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Pe Distance
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Ej Orientation
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Equatorial view
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Finvars
Finish BaseFunction
Int 2
Orbit False
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Handle Earth
Handle Venus
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Ch. plane vel.
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Graph projection
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Scale to view
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Advanced
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Prograde vel.
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Eject date
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0 -1874.86161265
Ch. plane vel.
0 706.17
Finvars
Finish BaseFunction
Int 4
Orbit True
Vector 1618689683.5 -1103954048.36 -5807348466.08
Vector -2815.01602124 1904.85245412 9992.11485299
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Finish BaseFunction
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Orbit True
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Outward vel.
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Ch. plane vel.
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Intercept with
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Advanced
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Velocity.
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Inc. angle
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Finish BaseFunction
Int 4
Orbit True
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Vector 5545.78451605 -919.395438935 9737.6148833
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Handle NULL
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Finvars
Finish BaseFunction
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Outward vel.
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Ch. plane vel.
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Intercept with
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Scale to view
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Inc. angle
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Eject date
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Finvars
Finish BaseFunction
Int 4
Orbit True
Vector -9282014526.3 -300140.518199 -95587669.1173
Vector 11236.904701 0.872802617346 101.245723706
Double 3.98600439969e+014
Double 43014.0445773
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Finish BaseFunction
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Orbit True
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Inc. angle
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Finish BaseFunction
Int 4
Orbit True
Vector -380184574253 37147804818.5 -302777387764
Vector 4407.16404346 -430.606879142 3495.73679095
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Handle Jupiter
Handle NULL
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Ch. plane vel.
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Finvars
Finish BaseFunction
Int 3
Orbit True
Vector -548574899050 11215729397.7 590807729058
Vector -15344.4031391 784.294173726 -9239.49660971
Double 1.32839126489e+020
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Handle Jupiter
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Inc. angle
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Eject date
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Finvars
Finish BaseFunction
Int 4
Orbit True
Vector 492253875804 -22609329132.2 159347332427
Vector -8034.13866963 370.189994487 -2625.14056218
Double 3.79311866084e+016
Double 44255.0704265
Handle Saturn
Handle NULL
Handle NULL
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Finvars
Finish BaseFunction
Int 3
Orbit True
Vector -1.38517255948e+012 62025840168.2 -394003471377
Vector -5667.23642331 156.587176915 -6061.43047578
Double 1.32750371142e+020
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Handle Sun
Handle Saturn
Handle Earth
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Outward vel.
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Intercept with
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Velocity.
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Inc. angle
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Eject date
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Finvars
Finish BaseFunction
Int 5
Orbit True
Vector 21196496495.7 -11075454045.8 -56549060445.6
Vector -4690.07178059 2407.62035168 12266.3296741
Double 3.98600439969e+014
Double 51133.0889618
Handle Earth
Handle NULL
Handle NULL
Select Target
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Prograde vel.
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Man. date
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Outward vel.
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Intercept with
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Scale to view
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Advanced
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Draw Base
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Finvars
Finish BaseFunction
END_MFD
BEGIN_MFD Right
TYPE User
MODE TransX
END_MFD
BEGIN_SHIPS
3:DeltaGlider
STATUS Landed Earth
BASE Cape Canaveral:1
POS -80.6758964 28.5227640
HEADING 75.00
RCSMODE 0
AFCMODE 7
PRPLEVEL 0:1.000000 1:1.000000
NAVFREQ 0 524 84 114
XPDR 6
GEAR 1 1.0000
PSNGR 2 3 4
TRIM 1.000000
AAP 0:0 0:0 0:0
END
END_SHIPS
BEGIN_VistaBoost
END
Repaired scenario:
Code:
BEGIN_DESC
Trajectory for imaginary Apollo 16 mutiny to fly to Venus Earth Earth Jupiter Saturn then Earth. Final encounter speed of around 13 km/sec.
END_DESC
BEGIN_ENVIRONMENT
System Sol
Date MJD 41423.6630600003
END_ENVIRONMENT
BEGIN_FOCUS
Ship 3
END_FOCUS
BEGIN_CAMERA
TARGET 3
MODE Cockpit
FOV 60.00
END_CAMERA
BEGIN_MFD Left
TYPE User
MODE TransX
Ship 3
FNumber 13
Int 1
Orbit True
Vector 5581601.93658 2686331.07021 1489679.95548
Vector -21.7463828367 -162.190146244 373.956888956
Double 3.98600439969e+014
Double 41423.6630599
Handle Earth
Handle NULL
Handle NULL
Select Target
0 Escape
Autoplan
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Plan type
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Plan
0 1
Plan
0 0
Plan
0 0
Select Minor
0 None
Manoeuvre mode
0 0
Base Orbit
0 0
Prograde vel.
0 0
Man. date
0 41423.6630599
Outward vel.
0 0
Ch. plane vel.
0 0
Intercept with
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Orbits to Icept
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Graph projection
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Scale to view
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Advanced
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Pe Distance
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Ej Orientation
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Equatorial view
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Finvars
Finish BaseFunction
Int 2
Orbit False
Handle Sun
Handle Earth
Handle Venus
Select Target
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Autoplan
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Plan type
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Plan
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Plan
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Plan
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Select Minor
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Manoeuvre mode
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Base Orbit
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Prograde vel.
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Man. date
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Outward vel.
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Ch. plane vel.
0 0
Intercept with
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Orbits to Icept
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Graph projection
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Scale to view
0 0
Advanced
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Prograde vel.
3 -4667.1620472
Eject date
2 41423.7351052
Outward vel.
4 -1938.09830909
Ch. plane vel.
3 708.5
Finvars
Finish BaseFunction
Int 4
Orbit True
Vector 1624756875.04 -1099347103.69 -5806529628.77
Vector -2828.18523053 1898.36671223 10000.1776043
Double 3.2485863e+014
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Autoplan
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Ch. plane vel.
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Intercept with
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Orbits to Icept
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Scale to view
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Finvars
Finish BaseFunction
Int 3
Orbit True
Vector 27324505767.7 -3000121645.96 -105298556443
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Inc. angle
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Finish BaseFunction
Int 4
Orbit True
Vector -4572895896.74 758722395.998 -8042262167.07
Vector 5530.29332363 -921.684947623 9753.33440014
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Int 3
Orbit True
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Outward angle
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Int 4
Orbit True
Vector -9281738463.15 -297455.53503 -119930989.445
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Handle Earth
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Int 3
Orbit True
Vector 142460480906 -1178721.6451 -49895928628.7
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Int 4
Orbit True
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Handle Jupiter
Handle NULL
Handle NULL
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Finish BaseFunction
Int 3
Orbit True
Vector -551148842954 12391374832.5 587892385667
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Handle Jupiter
Handle Saturn
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Finvars
Finish BaseFunction
Int 4
Orbit True
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Vector -8021.89290963 370.719326393 -2625.51285925
Double 3.79311866084e+016
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Handle Saturn
Handle NULL
Handle NULL
Select Target
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Outward vel.
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Ch. plane vel.
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Intercept with
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Orbits to Icept
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Scale to view
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Advanced
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View Orbit
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Finvars
Finish BaseFunction
Int 3
Orbit True
Vector -1.3847326649e+012 62028886910.4 -395872879933
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Handle Sun
Handle Saturn
Handle Earth
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Intercept with
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Finvars
Finish BaseFunction
Int 5
Orbit True
Vector 3363134115.4 -1769076944.94 -8470511235.4
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Handle Earth
Handle NULL
Handle NULL
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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
3:DeltaGlider
STATUS Landed Earth
BASE Cape Canaveral:1
POS -80.6758964 28.5227640
HEADING 75.00
RCSMODE 0
AFCMODE 7
PRPLEVEL 0:1.000000 1:1.000000
NAVFREQ 0 524 84 114
XPDR 6
GEAR 1 1.0000
PSNGR 2 3 4
TRIM 1.000000
AAP 0:0 0:0 0:0
END
END_SHIPS
BEGIN_VistaBoost
END
---------- Post added at 03:11 PM ---------- Previous post was at 08:27 AM ----------
I went ahead and flew it. The arrival back at Earth had an encounter speed of about 11km/s which translated to a bit over 15 km/sec at the Pe. Here's a screen cap of arriving. (click to enlarge)
What was interesting was on the initial departure from Earth, the trajectory on takeoff had a great view of the moon Venus and Saturn lumped together, and on the eject from LEO, the trajectory had me going past the moon fairly close to it. I was worried it would mess up the plan to Venus but it was far enough to cause minimal damage to the course.