23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.6326074515472915---------------------------
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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: 2023-04-19T15:26:50.513
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Launch V∞: [6.053942663871926, -7.75787335082349, -0.8954090939646077] km/s
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Phase 1:
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Planet: Saturn
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V∞_in: [2.2413327141582066e-6, -1.1187380207605594e-6, -1.8892705885870113e-6] km/s
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V∞_out: [3.07942187865685e-6, -4.0137174789414755e-7, 4.337256611566162e-7] km/s
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time of flight: 1.5649929630528867e8 seconds
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arrival date: 2028-04-03T23:28:26.513
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thrust profile: [0.31230009181042034 -0.14507517071179873 -0.1109127587109778; 0.16196849831184132 0.01705892450356684 -0.15382049363140668; 0.14649389947083885 0.05293273632884719 -0.20666903523953556; 0.13138526510449794 0.07100102555939396 -0.23947598350037194; 0.0884227168328481 0.05934787328281121 -0.20932335522131476; 0.032979047243451326 0.029498351395003945 -0.12183204854364776; 0.04685742838293943 0.060405621719852844 -0.13141210555658014; 0.021864074857883355 0.025525770864891592 -0.0778567553430435; 0.005739844543822382 0.011758496199014229 -0.020973220698547144; -0.005508268134433815 0.0022351875424058195 -0.002740632154001145; -0.008935564560123305 -0.03415586922936796 -0.003952409783786866; -0.004402660116607509 0.004436517438223065 0.024943014364053176; -0.011708072683526468 -0.02091574568506933 0.03634120772621851; 0.045516700194362235 0.05400180480869916 -0.003574012745101591; 0.009721950626811679 0.01616763771379539 -0.0473574351433496; 0.0072828665988345495 -0.003629292688263702 -0.03303709866673264; 0.04136207370066108 -0.038467322042712915 0.0010364520286586507; -0.03621757351235165 -0.17974900981628383 -0.13271610996248823; 0.04725612706285136 0.24128764125152674 0.013090112274600423; 0.06896550425790643 0.13859946481962915 0.005749343196023094] %
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Mass Used: 168.4953209277205 kg
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Launch C3: 97.6365781504205 km²/s²
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||V∞_in||: 3.1375930984675114e-6 km/s
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