archive/ES_0.5659004657678063---------------------------

Spacecraft: mySat
	dry_mass: 200.0 kg
	specific impulse: 3200.0 kg/s
	max_thrust: 0.00025 kN
	num_thrusters: 1
	duty_cycle: 1.0
Launch Mass: 3500.0 kg
Launch Date: 2023-04-29T11:05:53.999
Launch V∞: [6.329583756949594, -7.343839193818359, 0.12193457054396142] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [-3.6103217850726247e-7, -7.929224432336087e-8, 1.008063975436148e-7] km/s
	V∞_out: [-3.7746082231336006e-7, 3.38230628615429e-8, -4.870331248035376e-8] km/s
	time of flight: 1.855897541988334e8 seconds
	arrival date: 2029-03-16T11:48:27.999
	thrust profile: [0.5100142170924019 -0.12671791947305108 -0.14956292277917516; 0.10259295191925687 0.03191243953798148 -0.0997772042469217; 0.040903791908725826 0.026156928795549633 -0.07140410573266817; 0.03623019920034946 0.030216176832335608 -0.0865856342864938; 0.0780011184272211 0.06911165862190564 -0.21636807950740453; 0.021081629996324854 0.027526176734413096 -0.0849634392542505; 0.014365967983917502 0.01781881714858471 -0.07286634026119973; 0.007202474165715162 0.008331377800448628 -0.035216796709588306; 0.011637454090727938 0.012049190706501728 -0.057327443936936305; 0.007953995781026105 0.009915614297201171 -0.04697432976263949; 0.0015250393206034006 0.001441677263938496 -0.0077168787393373205; 0.0004816448529322344 -0.000420120659447595 -0.004824459402278755; 0.0010000381838058494 0.005030841506464517 -0.001378068236668261; 0.0004225803691851474 0.003545320700034086 -0.008832428324037753; -0.0008476754004438868 -0.0024099333482193786 -0.003235175335452723; 0.002053853505114232 -0.0016814436956492395 0.010967264316681819; 0.0014479985685253946 0.0030546160116196428 -0.01631447824022901; 0.001032149047349065 0.0036774709699410515 -0.012168532938361558; -0.00034188587383355174 0.002365626420146341 -0.004455627292661393; -0.003273513432437732 0.002309858889363173 0.00042601256428412976] %

Mass Used: 111.82278609346076 kg
Launch C3: 94.01047268039656 km²/s²
||V∞_in||: 3.8313629913290217e-7 km/s