30 lines
3.5 KiB
Plaintext
30 lines
3.5 KiB
Plaintext
/home/connor/projects/thesis/archive/EMS_2022-03-31T04:30:39.913/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: 2023-06-21T16:11:12.531
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Launch V∞: [4.580336710876162, -6.364445263085335, -1.5059609900586743] km/s
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Phase 1:
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Planet: Mars
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V∞_in: [5.6917792297860474, -9.107059519584473, 0.42920737253007657] km/s
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V∞_out: [3.8594088914119493, -9.999999222371288, 0.7899882429600399] km/s
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time of flight: 5.002931587226731e7 seconds
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arrival date: 2025-01-20T17:13:07.531
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thrust profile: [0.04229136644598212 -0.06399982439053087 -0.013233794183699233; 0.0014932116715965543 -0.004640304886228213 0.0001906966014413458; 0.0033744085280022597 -0.03336977966228066 0.005257073291176034; 0.0012173486808959046 -0.01856084430561746 0.006863306751990301; 0.0013367745067847335 -0.022179557580296334 0.01087995653246621; 0.0036625606619242286 -0.03753302445241814 0.02081824310414169; 0.005693436492274217 -0.04580963409486636 0.029614451707897785; 0.005714572044249225 -0.03497915028431355 0.027438168635040377; 0.003777208567280123 -0.02455099654485904 0.024014082477313365; 0.0017502727856114895 -0.013492983296062076 0.01677139465178059; 0.0014099722203796145 -0.02258436533622781 0.03086001815589659; -0.01711851756208839 -0.038162800905698104 0.06682067973653377; -0.07222108528125802 -0.044777544067508016 0.10793792074870515; -0.14908606147640172 -0.0461559607802597 0.1385554662454927; -0.23264661878032608 -0.05133863711785919 0.1564008191048521; -0.3111436864129761 -0.06543015638494414 0.16185133869771157; -0.3775737086759714 -0.0908253829695217 0.1565721147762051; -0.4298924012671283 -0.128999814797943 0.14270289395075253; -0.4643281358807509 -0.17906953537930623 0.12257663575791145; -0.4706052520449254 -0.22992815837368674 0.09655625247918113] %
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Phase 2:
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Planet: Saturn
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V∞_in: [-2.246348693769835e-6, 2.3753426785927334e-7, 2.5288257778483175e-6] km/s
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V∞_out: [-2.516669621821466e-6, -6.463053739261209e-7, 2.0443342168870033e-6] km/s
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time of flight: 1.9486152593971774e8 seconds
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arrival date: 2031-03-26T01:25:12.531
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thrust profile: [-0.17633532461638057 -0.9999797294136397 0.015024325195942026; 0.9999986736375168 -0.9999918362728258 -0.1360686231839698; 0.9999988035500681 0.2439734687302935 -0.11913834595120573; 0.9999986251683992 0.8682898739883735 -0.11093379400311718; 0.9999994614450388 0.9999929666195986 -0.09303791503519601; 0.7673577770891561 0.9999839849865495 -0.06846222282089853; 0.42997221568724037 0.8288852823182677 -0.045830355401957935; 0.18215854580869686 0.4905856393977488 -0.025668582879886326; 0.030437897869578262 0.1150455831440398 -0.0044169993998817375; 0.000807513276163115 0.004402642329890393 -0.0004919165276516808; -2.7745989651617884e-6 0.00012024951636535067 5.147622876497583e-6; 4.877668061774889e-5 0.0002184086121649586 8.498500131050681e-6; 4.132626798573495e-5 8.138845277836206e-5 -3.472982010536854e-5; -6.0757100897981974e-5 0.00012392554025281714 2.6509457699324238e-5; 0.00018725736157467317 6.848523112973848e-5 6.68862906209139e-5; 3.3549665625494406e-5 0.00011153259853957193 -5.104946327333131e-5; -4.4178366374466365e-5 3.558251004156073e-5 -1.1982307674649479e-5; -0.00013762482047567344 1.3746134754174806e-5 -2.093755807885032e-6; 4.771811294273377e-5 4.731274921606212e-5 -1.1671493023451763e-5; 7.19639059100438e-5 -0.00013724663359736313 -3.071142693588584e-5] %
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Mass Used: 771.0879580725491 kg
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Launch C3: 63.75356639538772 km²/s²
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||V∞_in||: 3.390791175687325e-6 km/s
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