archive/ES_0.5627280250016633---------------------------

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: 2023-04-29T07:43:37.459
Launch V∞: [6.375824807848056, -7.342536790196925, 0.06325529633420743] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [1.1763925411846936e-5, 1.5366515022646352e-6, -3.2643191537090305e-8] km/s
	V∞_out: [-2.2926597119883233e-6, 5.249697875676675e-8, 1.1638721034104606e-5] km/s
	time of flight: 1.874957778750514e8 seconds
	arrival date: 2029-04-07T09:53:14.459
	thrust profile: [0.39432594092791495 -0.07735239886341229 -0.11453618319979827; 0.1683014999668032 0.06438671064447887 -0.1540308505075896; 0.09298831297011617 0.06750194425481763 -0.14873927554845776; 0.037635711573166974 0.03572334246156351 -0.08639812249357338; 0.03540579898570081 0.04205340393120068 -0.10602809208445285; 0.021980287454700643 0.03138756468758215 -0.0869875631960744; 0.023448216496487973 0.04383357193608814 -0.11543865320678419; 0.013695963516784588 0.02117430584479244 -0.06307160317478787; 0.004072196482905346 0.008444765341001017 -0.02640597165567753; 0.0005380442086528856 0.0012839334915132495 -0.004356371687124506; 0.001779637607948029 0.004417313508336477 -0.017689519892169447; 8.610750139515153e-5 4.869177097914476e-5 -8.253670346739601e-5; 2.7370600051500073e-5 8.578330516399908e-5 -0.00027454262283109477; 1.2804980448886055e-5 2.7363130722441364e-5 -0.00010545377078272701; -2.7575525793696034e-5 -0.00016659349161551103 -0.0001925482466388747; -1.4278512877641474e-5 7.598051159206609e-5 -0.00015189796164150952; -0.00010176706334491531 0.0001998883583341073 -0.00021545512053335866; 0.00016960766728823438 0.0002223443392688959 -0.00034028496395594577; -0.0001419844935122011 0.00011899346623932082 -0.00010595050662395064; 2.5806389745332108e-5 -1.4587397664998222e-5 6.575912540373783e-5] %

Mass Used: 104.869422420305 kg
Launch C3: 94.56798972828038 km²/s²
||V∞_in||: 1.1863907640944613e-5 km/s