Hyperbolic Departure & Flyby Orbits
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Hyperbolic Departure Orbit from Kerbin
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Semi-major Axis =               -1534.129 km
Eccentricity =                  1.454529743
Inclination =                   13.133 deg
Right Ascension of AN =         167.495 deg
Argument of Periapse =          353.468 deg
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Out. Hyp. Vel. Unit Vect X =    0.417573046
Out. Hyp. Vel. Unit Vect Y =    -0.890291705
Out. Hyp. Vel. Unit Vect Z =    0.181695987
Out. Hyp. Vel. Magnitude =      1.517241842 km/s
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Inbound Hyperbolic Flyby Orbit to Eve
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Semi-major Axis =               -725.734 km
Eccentricity =                  3.2981
Inclination =                   152.775 deg
Right Ascension of AN =         125.180 deg
Argument of Periapse =          115.344 deg
Periapse Radius =               1667.840 km
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Outbound Hyperbolic Flyby Orbit from Eve
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Semi-major Axis =               -725.734 km
Eccentricity =                  3.2981
Inclination =                   152.775 deg
Right Ascension of AN =         125.180 deg
Argument of Periapse =          115.344 deg
Periapse Radius =               1667.840 km
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Inbound Hyperbolic Orbit to Moho
---------------------------------------------
Hyperbolic Excess Vel. =        2.549 km/s



Sun-Centric Transfer Orbits
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Phase 1 Transfer Orbit (Kerbin -> Eve)
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Semi-major Axis =             10506615.769 km
Eccentricity =                  0.294506169
Inclination =                   2.026 deg
Right Ascension of AN =         27.509 deg
Argument of Periapse =          178.904 deg
Period =                     6249549.1312 sec
Departure True Anomaly =        181.096 deg
Arrival True Anomaly =          94.171 deg
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Phase 2 Transfer Orbit (Eve -> Moho)
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Semi-major Axis =              7876536.836 km
Eccentricity =                  0.356538814
Inclination =                   5.675 deg
Right Ascension of AN =         99.766 deg
Argument of Periapse =          53.970 deg
Period =                     4056555.0494 sec
Departure True Anomaly =        146.943 deg
Arrival True Anomaly =          42.744 deg
---------------------------------------------
Kerbin Departure Date =
                Year 2, Day 246 04:48:55.171
                       (14510935.171 sec UT)
Eve Arrival Date =
                 Year 3, Day 12 03:07:17.774
                       (18652037.774 sec UT)
Moho Arrival Date =
                Year 3, Day 148 05:13:22.345
                       (21597202.345 sec UT)
---------------------------------------------
Total Mission Duration =
                       328 Days 00:24:27.174



DV Maneuver Information

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Burn Information to Depart Kerbin
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Total Delta-V =                 1.440 km/s
Prograde Delta-V =              1174.236 m/s
Orbit Normal Delta-V =          798.026 m/s
Radial Delta-V =                237.679 m/s
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Burn True Anomaly =             167.495 deg
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Burn Information to Depart Eve
---------------------------------------------
Total Delta-V =                 0.000 km/s
Prograde Delta-V =              -0.000 m/s
Orbit Normal Delta-V =          -0.000 m/s
Radial Delta-V =                0.000 m/s
---------------------
Burn True Anomaly =             0.000 deg
---------------------------------------------
Total Mission Delta-V =         1.440 km/s