archive/ES_0.5838744572748303---------------------------

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: 2023-04-28T08:11:15.155
Launch V∞: [5.6728877009779515, -8.34485134571389, -0.8428678656232316] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [8.846556087690508e-6, 0.008757084191035101, -0.0029179838518313453] km/s
	V∞_out: [-0.007486759036999347, -0.004092366773335758, 0.003521670002916212] km/s
	time of flight: 1.5019171024433386e8 seconds
	arrival date: 2028-01-30T16:06:25.155
	thrust profile: [0.03493914294397491 -0.0241649791939514 -0.020901127240890414; 0.04242444986931142 -0.008952064176163557 -0.06262463006631976; 0.0565766734968723 -0.007180128445983821 -0.14111658128661816; 0.052014772933356226 -0.006372581386922036 -0.17944365489045158; 0.04444241259396148 -0.006498489505910236 -0.1916443861370839; 0.035894383866374724 -0.006350380342112578 -0.1812967723175921; 0.02734608970905313 -0.005625260881460439 -0.1548456986482449; 0.02019564249359045 -0.004732065416424391 -0.12481555730339161; 0.011671760628656252 -0.003005265954187342 -0.0753363880776184; 0.0049390852913840716 -0.0018699308168766402 -0.030024305202656427; 0.002240256369627856 -0.0001274441269402131 -0.016296125463579787; -0.003036639340017806 0.0030885100920935685 -0.009080664590475573; -0.0015539035460527598 0.0024543176241988043 -0.020282705986412262; 0.009692681516686008 -0.007923491750403308 0.005793653538518826; -0.005736395257116187 0.0030123814706328684 -0.010102530930735393; 0.003787217961063529 -0.0032540502038494695 0.0026081989998519104; -0.005019016554605379 0.006119105239581826 -0.027297814901854164; -0.012312881425439704 0.005500477679446816 -0.0036198994066769484; 0.00465867687965833 -0.005052610111701096 -0.028589133391627324; -0.003458887962152434 -0.0012616063524272946 0.0021869956649622803] %

Mass Used: 83.10322046889314 kg
Launch C3: 102.5286250888701 km²/s²
||V∞_in||: 0.00923045131886735 km/s