archive/ES_0.5658220202611646---------------------------

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: 2023-04-28T02:00:10.678
Launch V∞: [5.900820760574823, -7.684078327993536, -0.021626626753506885] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [3.9853009959873635e-7, -2.145815714485665e-7, -3.599799122678099e-7] km/s
	V∞_out: [2.457081378213536e-7, -3.5750890318595504e-7, 3.8247287224528777e-7] km/s
	time of flight: 1.7366006988004687e8 seconds
	arrival date: 2028-10-28T00:54:39.678
	thrust profile: [0.4773230059096041 -0.1651049810985121 -0.17248228353912212; 0.19102939801072705 0.037593010106696814 -0.19951265085700437; 0.05823329797425824 0.025443293645817273 -0.10619652033049845; 0.04281054708477046 0.025851010047054937 -0.10747992558045273; 0.033367185386307195 0.024351173489366853 -0.1034580774516903; 0.026596856791959812 0.022990234259556288 -0.10215424908282032; 0.03358130814452016 0.029970623959581087 -0.14155760545332993; 0.008179294872162603 0.007985777706431033 -0.040417797742834105; 0.00955932203860434 0.010129774072541307 -0.05275187669546481; 0.008463778106071636 0.009623613082990272 -0.05208082437218412; 0.004370082799333873 0.005194910193600545 -0.029182515781031648; 0.0023557384791899312 0.0035283481136207055 -0.018303727255260274; 0.0001807212815036536 -0.000263851196468699 -0.0013887037607256381; 0.00010991993004005575 0.0005234141649449823 -0.0014533037004347852; 0.0002058789263104416 0.0001435709130452021 -0.0008113816747071568; 0.0003055748675759957 8.987353940919746e-5 0.0001851196934871172; -0.00011781468729514717 -2.0742652053619892e-5 0.00022733944894699377; -0.00038083750362072235 0.00024659008051572027 0.0007060691699515447; 5.9195561675215403e-5 0.00012024606986534687 -0.0006408201728977793; -0.00014354209270694247 -0.0002458670824791063 -0.0002705582538792984] %

Mass Used: 112.57861382878491 kg
Launch C3: 93.86521311015551 km²/s²
||V∞_in||: 5.783225988389655e-7 km/s