archive/ES_0.5946647125886267---------------------------

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: 2023-04-17T07:21:46.489
Launch V∞: [6.367577588268499, -7.0831709083419945, 0.3361212594169347] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [9.934426859218278e-8, 2.511798858474229e-8, -3.264965523246944e-8] km/s
	V∞_out: [1.0380714277330518e-7, -2.7774505297052966e-8, 1.3362474098288573e-8] km/s
	time of flight: 1.856295965153089e8 seconds
	arrival date: 2029-03-04T19:08:22.489
	thrust profile: [0.7258968795842917 -0.1847696729986004 -0.10265074169141086; 0.4424206315844121 0.17199466395018218 -0.19771856386105674; 0.16902081993610416 0.13130200571303774 -0.14787006239854397; 0.18043626895772055 0.19012179530494988 -0.20945606779011172; 0.078517489350667 0.10753455579432926 -0.12803951570368227; 0.027499463630528825 0.04712820459013554 -0.06113785774581906; 0.011177923553285061 0.021682387732792217 -0.02950682755367616; 0.0016078885280501995 0.0035256939555137084 -0.005088850312694682; 0.005893360005382827 0.01394471343673791 -0.020142640075674987; 0.0005814230195868483 0.001646609398035615 -0.00234064015493265; 0.001931386336834468 0.0056642645593629375 -0.00893765783106512; 8.345816876242297e-5 0.00013257772331491956 -0.0002546339104865126; 3.9909855646392064e-5 -3.0875087805004022e-6 -8.363856422941487e-5; 0.0001374369720853893 0.00011664917723697626 -0.00014794204423541224; -4.8244167350951694e-5 1.3356342875673938e-5 -9.578731473266594e-5; 4.856621559128674e-5 1.709403590676531e-5 1.3378546754088517e-5; -5.542493784747969e-6 0.000137453042880943 0.0001474665534228906; 0.00021150518249481867 8.7381697603749e-5 -0.0001016253200255684; -9.637757583864974e-6 -7.669034155294887e-5 0.0001438588215496624; 3.513186829794622e-5 0.00026628283148673397 3.3018974496926406e-5] %

Mass Used: 163.93189491753492 kg
Launch C3: 90.83033196043365 km²/s²
||V∞_in||: 1.0754625534837612e-7 km/s