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(W/ only planet-centered portion of entire mission)
The latest iteration of the JIMO mission will be used to define this reference case.
Callisto to Ganymede to Europa:
NEP Gross Power 190 [KW]
Isp = 7000[s]
NEP total efficiency = 70
Duty Cycle = 98%
During Europa spiral down portion:
NEP Gross Power 190 [KW]
NEP total efficiency = 44.0974
Isp = 2280.898900 [s]
Starting State: Science Orbit Around Callisto
JD 2459954.4532 (January 9, 2023 22:52:34)(FIXED)
Initial Mass [kg] = 29505.7978 (FIXED)
Semi-major axis 2503.470677 [km]
Eccentricity 0.6150127125E-02
Inclination 108.9040100 [deg]
Long. Asc. Node -19.03598938 [deg]
Argument of Peri. 18.38213649 [deg]
True Anomaly -177.6023427 [deg]
State at Ganymede Science Orbit:
JD 2460538.2549 (August 15, 2024 18: 7: 3)(FIXED)
Mass [kg] = 27724.1897
Semi-major axis 2734.060425 [km]
Eccentricity 0.1860901876E-02
Inclination 109.7135359 [deg]
Long. Asc. Node 149.8346378 [deg]
Argument of Peri. -60.70937538 [deg]
True Anomaly -179.0244771 [deg]
State at Europa Science Orbit:
JD 2460920.2400 (September 1, 2025 17:45:35)(FIXED)
Final Mass [kg] = 25093.3063
Semi-major axis 1665.452543 [km]
Eccentricity 0.6416612797E-02
Inclination 109.0719444 [deg]
Long. Asc. Node -113.0932876 [deg]
Argument of Peri. 112.8494976 [deg]
True Anomaly -52.72015937 [deg]
Overall Performance:
Initial Mass [kg] = 29505.7978 (FIXED)
Final Mass [kg] = 25093.3063
Propellant Mass [kg] = 4412.4915
TOF [days] = 965.7868
Originally modeled using Mystic
Input/Output files
Mystic9_0_0.zip (download)
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