30 lines
3.5 KiB
Plaintext
30 lines
3.5 KiB
Plaintext
/home/connor/projects/thesis/archive/EMS_2021-12-11T12:00:40.323/mission---------------------------
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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: 2024-12-15T15:53:57.209
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Launch V∞: [-8.799630990613117, 7.34551872539945, -0.01567157263418129] km/s
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Phase 1:
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Planet: Mars
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V∞_in: [-5.525424782477056, 4.4780198756447795, 4.819122758622572] km/s
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V∞_out: [-4.706421743487455, 5.965879679145328, 4.008068881526253] km/s
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time of flight: 3.454176957567771e8 seconds
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arrival date: 2035-11-26T13:15:32.209
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thrust profile: [-0.3626481337773754 0.04577398887343224 -0.01655095159279829; -0.2591029103072647 0.1372224625894388 -0.03484794687568234; -0.22866525688135636 0.17047902428739029 -0.04398596135663903; -0.20591128156544064 0.17475285966822163 -0.0492888779248724; -0.18150056503077222 0.16778930777145082 -0.052511568277184374; -0.15335231896039642 0.1563088671676009 -0.05489695682401099; -0.11969538605349696 0.14368122907327513 -0.057381477632554384; -0.07554857095074854 0.13274289955008667 -0.061134164848177484; -0.005662845372976561 0.12158533590493402 -0.06883945566112469; 0.08882737363292448 0.08080812675137844 -0.06713978489287248; 0.14973273476648047 0.012685076152274712 -0.054648024648829695; 0.18323594004050148 -0.016384245272972057 -0.040066936961717516; 0.214348858008005 -0.03857066861559532 -0.03192224738926298; 0.2437677883438544 -0.05412293733006518 -0.024660532031911552; 0.2708260597859475 -0.0661687448280918 -0.017461136277209074; 0.2929814040329991 -0.06841327312791493 -0.01010361901238175; 0.3092263370993894 -0.06754436134630445 -0.002601950724966861; 0.3149711596447107 -0.06392107998759775 0.004480656365829517; 0.29966216490402514 -0.07283217119754073 0.007976136077309862; 0.2774497080818675 -0.23673465946359637 -0.020355523705770436] %
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Phase 2:
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Planet: Saturn
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V∞_in: [-3.3584183538877763, 3.8318829241241077, -0.7567106147040691] km/s
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V∞_out: [0.1021866916167663, -0.00023345092684676295, -0.009051525807691481] km/s
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time of flight: 1.543622855088476e8 seconds
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arrival date: 2040-10-17T03:40:17.209
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thrust profile: [0.13343967665884301 -0.10506545000498568 -0.0477351077659778; 0.1302117419653648 -0.03935460102717447 -0.05153213061680276; 0.11177284747102363 -0.01257220530234715 -0.04992659428886335; 0.09652693312293067 -0.002381618439009866 -0.04765269265520941; 0.0850825371473891 0.0014317391384792745 -0.04538853860191621; 0.0764692224980894 0.002389375863760724 -0.043313336682117246; 0.06984581101704013 0.001982743995643555 -0.04109653594773106; 0.06469926152021455 0.0007704842623266529 -0.03917176815195523; 0.06065861914276538 -0.0009274805284651806 -0.03711303987104724; 0.057503566679394116 -0.003082072948930367 -0.034909201620028106; 0.0550645718937643 -0.005650610120539781 -0.03268940722476422; 0.05322150250858926 -0.008613752406916884 -0.030366444716783268; 0.0518961775636053 -0.012130900432895326 -0.027730459432375138; 0.05102478831673343 -0.01609208695110308 -0.02458927158108588; 0.05053365271120057 -0.02060666132173175 -0.02046187508115701; 0.05010304886930772 -0.024812286823873268 -0.01532028206532522; 0.04934671183992039 -0.028238984577646484 -0.009343074776168988; 0.04800853819288795 -0.030411131488611035 -0.0034811661314590016; 0.046080118190868546 -0.03168857673917387 0.0018689351571204262; 0.04350626131303775 -0.03258848698710888 0.006743047916297395] %
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Mass Used: 794.3057297478713 kg
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Launch C3: 131.3903965143416 km²/s²
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||V∞_in||: 5.1512048627801645 km/s
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