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archive/ES_0.566660208433267
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archive/ES_0.566660208433267---------------------------
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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: 2023-04-27T03:12:40.657
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Launch V∞: [6.249697536696187, -7.6347521832392875, -0.12834747579293726] km/s
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Phase 1:
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Planet: Saturn
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V∞_in: [-2.2101722734997827e-10, -3.2267023537680095e-9, -1.138471054030397e-8] km/s
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V∞_out: [4.212222327271077e-9, 6.260961991551913e-9, 3.030310487548594e-9] km/s
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time of flight: 1.7347157221127862e8 seconds
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arrival date: 2028-10-24T21:45:32.657
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thrust profile: [0.2061363546969812 -0.07500139584650536 -0.07740777381827085; 0.08641100657920178 0.01403849391723832 -0.09006926410304805; 0.09519638607071387 0.03790028034523942 -0.16212872149815524; 0.07912193592145894 0.04398004251634266 -0.1857295014399546; 0.08767555636363215 0.05970247478602815 -0.2593343664809706; 0.02995103012449217 0.02330675283610865 -0.10766471049919471; 0.021415877083247204 0.018406205415707557 -0.08978978421619639; 0.004250925923235643 0.004506620834213277 -0.020044092393378826; -0.001339783141691371 0.0030454267568239455 -0.00932006063086529; 0.0021008795031727916 0.000438519109853928 -0.004990963325045733; 0.002652691595190165 -6.0134362816092264e-5 -0.010653681514920542; -0.0022067762630272095 0.002266355398014658 -0.006775058227479023; 0.0009357615247013476 0.0003827189980932738 -0.00016990035443821333; 0.0039078811793508625 0.0017479575012494092 -0.005344740905174429; -0.006595643286542021 -3.107537805044445e-5 -0.004085720205998572; 0.0015342274257516876 -0.004105660137057009 -0.0001560476646769854; -0.003100494202699447 -0.00161394388951979 0.002454106263705905; 0.009119620672686495 -0.004354377530140315 -0.004250908425697297; -0.0007945784560334118 0.007480870846400091 -0.007904669484684096; 0.00045698596443463765 0.0010775889367350446 0.0021102131361455598] %
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Mass Used: 93.14321573927737 kg
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Launch C3: 97.36463327420587 km²/s²
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||V∞_in||: 1.1835205565646326e-8 km/s
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