23 lines
1.9 KiB
Plaintext
23 lines
1.9 KiB
Plaintext
archive/ES_0.6560723113930567---------------------------
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Spacecraft: mySat
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dry_mass: 200.0 kg
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specific impulse: 3200.0 kg/s
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max_thrust: 0.00025 kN
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num_thrusters: 1
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duty_cycle: 1.0
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Launch Mass: 3500.0 kg
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Launch Date: 2023-04-22T16:51:35.766
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Launch V∞: [5.378122230744136, -8.156115096554329, -0.46340916612132244] km/s
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Phase 1:
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Planet: Saturn
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V∞_in: [-0.0002064757995727344, 8.821226785561729e-5, -0.0002029358206482952] km/s
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V∞_out: [-8.077784022956258e-5, 0.0002004297210368016, 0.0002117815840040048] km/s
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time of flight: 1.4210995079587454e8 seconds
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arrival date: 2027-10-23T11:50:45.766
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thrust profile: [0.4494739265755561 -0.2632478722991777 -0.19015959420133685; 0.12267808214246351 -0.008836737982524143 -0.1089946519209061; 0.10231298979592575 0.01565935116678991 -0.14564108945992563; 0.09038099821737772 0.030353650859286915 -0.17993207719531668; 0.08359940286823897 0.0316875446308953 -0.1944264397028802; 0.06289127377950166 0.02870150155126642 -0.16725170790937022; 0.052844998825244904 0.007421046767492256 -0.08920813054808002; 0.1575947775558399 0.024485024084145733 -0.1603323845281368; 0.059381167834787654 0.000773572583705473 -0.16440341987543663; 0.04503163967477891 0.005267867805728381 -0.07389361919483337; 0.1200078802463998 -0.023816787121216883 0.0010121116414699254; 0.2338951883297835 -0.09861817282044846 -0.09304723322512436; -0.006841910371656337 0.004314199778677031 0.06737785210796868; 0.009499462476571045 -0.013804969423957383 -0.02547099585153692; 0.09643280667380355 -0.011909509871720353 0.003051194286260356; 0.021408162482172016 -0.0246471517523682 0.006845006065413106; 0.14372551384303567 -0.03966162116509232 0.05474156900909122; 0.1457800884351052 -0.11040078796780657 -0.023632746565111558; -0.16463824742043023 0.025421886040607425 -0.16949416521964972; 0.11580599628521202 0.05675899831301226 -0.3519536637120141] %
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Mass Used: 207.39426182008538 kg
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Launch C3: 95.66116025231098 km²/s²
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||V∞_in||: 0.0003026493140775776 km/s
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