archive/ES_0.5636547318138416---------------------------

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: 2023-04-27T19:55:36.082
Launch V∞: [6.525174726283663, -7.363380795773494, 0.25417725354213183] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [-2.873239134225585e-8, 6.053361169847948e-8, 3.348451364243676e-8] km/s
	V∞_out: [-1.8837874431228397e-8, 3.860007799675279e-8, -6.201381570196554e-8] km/s
	time of flight: 1.8389309343408552e8 seconds
	arrival date: 2029-02-23T05:20:29.082
	thrust profile: [0.22157577782097912 -0.05440254918487352 -0.06883067531383733; 0.14539387874096293 0.04608357129883673 -0.13200005908044354; 0.09558624048081306 0.05828000782435531 -0.14559663474278767; 0.07600437162942121 0.063471754764354 -0.16281597895721947; 0.05324531541111606 0.05505221420053832 -0.14930623242359453; 0.02487767265999587 0.035559862966206335 -0.10222460687097223; 0.0161270773517461 0.02657114261235965 -0.0816091512401934; 0.0064510906825551865 0.010988566665094712 -0.03805083631267255; 0.0025450904169699636 0.0038778997585429235 -0.01416593835331254; 0.0020068091287406523 0.003604327419453101 -0.013453324220642783; 0.001007369647851553 0.002061989704275879 -0.007577998959197408; 1.9685509112659222e-5 -0.00010276217476251455 0.00013075012464972154; 0.0004645665357584794 -0.00030232327268478096 0.0001496160000529271; -3.881228682176855e-5 2.1297138913942343e-5 0.0008209796202330877; -0.00023905191345980617 -0.00019536601600101566 0.00029729374533880913; 0.0004204972051081234 6.575326743468542e-6 0.00014973615554538894; -9.658714002300787e-6 -0.00031665168063214704 0.0008512699538504643; -1.706387247020445e-5 -0.0004825362729175762 0.0012301132118783939; -4.0558105154486423e-5 -0.00022591950234305543 -0.0005018581207751444; -0.0004758278361299518 -0.0005136473159531462 0.0013358376171689235] %

Mass Used: 92.56950695097657 kg
Launch C3: 96.86188802831519 km²/s²
||V∞_in||: 7.49071499349519e-8 km/s