archive/ES_0.5616520536051469---------------------------

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: 2024-05-11T05:30:41.641
Launch V∞: [7.822271555315889, -5.827453340361265, 0.0732785385546183] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [0.0028105379039113977, 0.001903361951547906, 0.11545952402128255] km/s
	V∞_out: [-0.1074966009692615, -0.03814268914817087, 0.01757502666849639] km/s
	time of flight: 1.8078011765712273e8 seconds
	arrival date: 2030-02-01T14:12:38.641
	thrust profile: [0.3768648384059129 -0.01585025002908052 -0.11695648554722411; 0.13313615751360547 0.07036740880803806 -0.1386565759698351; 0.08396852112744947 0.07277662202630729 -0.15553003575491037; 0.039696189022818476 0.04639860880927312 -0.11284318639214179; 0.04562374149056144 0.06719567705621717 -0.1717964814155304; 0.01605986810283878 0.02753762379064343 -0.07808866981815984; 0.010140668385577102 0.019540474054199723 -0.06059397953846552; 0.0022452181054934753 0.007045474563652964 -0.01829677800531339; 0.00030729057264815567 0.004491287720672511 -0.01355002224339383; -1.1032380613337518e-5 0.00029501769751120923 -0.0019399407082337826; 0.006234733357520242 0.007303034118560078 -0.0237550171748707; -0.0005486054179699737 -0.0004896229206001784 -0.0014860965840700767; -3.519843603010486e-5 -0.002702671515842671 0.0014061004843067986; -0.00029545433292382876 -0.00015925448443631892 0.003919263696771618; 9.082843183211091e-5 -0.0004129038121111848 -0.0015551074556038366; -0.014067798740543005 0.006054203336132703 -0.005201860403025411; -0.004113170551349338 -0.010717577932812968 -0.0029765314232230227; 0.0021857451206768255 0.0007269389418141997 -0.007650923840370064; -0.01225102967869281 -0.01152773130107946 -0.014356395686183604; -3.374942573591087e-5 0.00048742364656497486 -0.004094166193922694] %

Mass Used: 100.20439483614564 kg
Launch C3: 95.15251446340442 km²/s²
||V∞_in||: 0.11550940912864652 km/s