archive/ES_0.5607220886356743---------------------------

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: 2024-05-10T12:58:58.302
Launch V∞: [7.728365985817934, -5.793406038664955, 0.5098916663608258] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [5.72162344719778e-7, -1.955608391568761e-6, -6.3784741964032936e-6] km/s
	V∞_out: [-5.489884814439423e-6, -6.069324185758273e-7, 3.7799931887148e-6] km/s
	time of flight: 1.8088021668376046e8 seconds
	arrival date: 2030-02-02T01:29:14.302
	thrust profile: [0.5486947776323133 -0.027355380773924923 -0.13887614459433528; 0.0995825120765841 0.053998069839248077 -0.09701754373646451; 0.12479212309798282 0.11159497088513116 -0.20764448451396; 0.0216035448532328 0.02576981613319774 -0.06125712272444029; 0.025391994928014885 0.03780843942400175 -0.08934887674825107; 0.03315680045421173 0.05451560118849448 -0.13478048744098922; 0.007764617783942706 0.017262369905735073 -0.04936621881299695; 0.005269705396201126 0.013210359542475287 -0.0380127883410386; 0.001756563769102353 0.011209561013089921 -0.034112427513044746; 0.0022781210013356635 0.007776991366065494 -0.026187651837041078; -0.00022861154982969033 0.0011709558961051159 -0.004301669603932528; 0.0022581929617103676 -0.0006107203941500103 -0.002829385508710576; 0.0003644252803495929 0.0032042328683053204 -0.007371525983559501; -0.0018854882477625289 -0.0019476064645309907 0.004019422667786614; -0.0005762784464225686 0.00020212955105683748 0.00047199544048892204; -0.0008662664937482943 -0.0006386101111260445 -0.0008021646132482562; 0.002736013953908001 -0.0012034796366279157 -0.0012013430401973217; -0.0011677276191271416 -0.002655880709837216 -0.00355690638905072; 0.0018289189348541749 -0.0038780058848420862 -0.005153419244451769; -0.0013572496959509993 -0.002343997639648948 0.009189069478193337] %

Mass Used: 108.46053094405352 kg
Launch C3: 93.5511838510114 km²/s²
||V∞_in||: 6.6960217296594874e-6 km/s