archive/ES_0.5595343351181956---------------------------

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: 2024-05-10T08:43:51.933
Launch V∞: [7.839363459800086, -5.495167717078827, 0.41292618986744073] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [-1.8514103035216931e-9, -1.6194363719524026e-9, -1.3819723876269756e-9] km/s
	V∞_out: [-9.802442458629809e-10, 9.163439871146422e-10, -3.3794318558824427e-10] km/s
	time of flight: 1.8749577787468886e8 seconds
	arrival date: 2030-04-19T10:53:28.933
	thrust profile: [0.7103604904750775 0.013021485474621447 -0.18122621761632496; 0.13897166092789806 0.08834322463212221 -0.13459893567579734; 0.05075533865098167 0.05291952145644776 -0.0924473483288444; 0.051837508622697814 0.07350700905175718 -0.1409872892396794; 0.017926813842953616 0.03177904369868192 -0.06881067580954169; 0.015557423558885326 0.033538325306211855 -0.0782867750684514; 0.008833544111574318 0.022745892016046394 -0.05690731794544143; 0.006700550576970491 0.020956025004851813 -0.05528685324615177; 0.0012107202810360727 0.00437306830718111 -0.012769752294260325; 0.0011968941966324768 0.002428869074149822 -0.007888624356476298; 0.0008974778039163903 0.001576694433302677 -0.0048155539171806875; -7.716089107376363e-5 -0.0015728984418026354 -0.003953659478389724; -0.0011720442855192464 0.0002652933999484055 -0.002395523648975823; -0.0011040179187917793 0.0005823083667879929 -0.0032862308162201733; -0.0003106461065512245 0.004695727571565772 0.0011587313456062642; 0.0006513315838840488 0.0004469474921271849 -0.0008528616362925274; -0.0007962918482250824 0.0009837681722623171 -0.0006593404987457405; 0.0010272939587450548 1.185146154286925e-5 -0.0023201900094045134; -5.4003866673994674e-5 -8.487590407076561e-5 0.0006160314962912663; -0.0010735606489521983 0.0028976829413202157 0.002687168746831012] %

Mass Used: 117.15591586817163 kg
Launch C3: 91.82299573195255 km²/s²
||V∞_in||: 2.821372353120384e-9 km/s