archive/EMS_0.885200034193802---------------------------

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: 2024-09-20T14:03:44.662
Launch V∞: [-0.9544125442488793, 4.650055637860991, 0.8829883975591813] km/s
Phase 1:
	Planet: Mars
	V∞_in: [-2.686848874040082, 5.69557833738042, -0.3426867301634786] km/s
	V∞_out: [-5.006830246285463, 3.8244101442357286, -0.28590492992060296] km/s
	time of flight: 1.2959473202133252e8 seconds
	arrival date: 2028-10-29T12:35:56.662
	thrust profile: [-0.028074398281491695 0.03725829642101633 0.011493562796176157; -0.04057241823105847 -0.0036979634745522238 0.004188100162030408; -0.018576540265103334 -0.016670623079762328 -0.0036538504180610655; -0.00926818068907572 -0.029823872248843347 -0.00788998730301693; 0.0056536273790355335 -0.039471274595512786 -0.015505661293943124; 0.01795773380852956 -0.024832086810877792 -0.012157101567918709; 0.020276654954958836 -0.008918038755765955 -0.0074245383137495295; 0.026868221096269136 0.007263820280035479 -0.004654400052923847; 0.011894893359756988 0.03223774798632351 0.004633535267024402; -0.047141055295386355 0.040019079580037704 0.013364609633569504; -0.04520469085369964 -0.010120922532993988 0.0020777538652468844; -0.024235864777124916 -0.02628842319518715 -0.005178953753261158; -0.020104196631084845 -0.08663986569488229 -0.025957813503050115; 0.04562945777248198 -0.18858114469692783 -0.07388958835417316; 0.1654642046172344 -0.19639566019786459 -0.09899123711104271; 0.20836768567311814 -0.07684473602532182 -0.06621134288112417; 0.17451643722399424 0.054856569336227734 -0.019947666848185868; 0.09171150949789851 0.24766459803783164 0.03479747010758981; -0.23524183946575974 0.2601294101394598 0.07688820773607916; -0.21879974186036938 -0.008020833470565012 0.021595583194403873] %
Phase 2:
	Planet: Saturn
	V∞_in: [2.746703786000276, 2.98969776442552, -1.0550945579969648] km/s
	V∞_out: [-2.364529965587132, -1.1050142331661583, -3.0819068226828907] km/s
	time of flight: 2.2586692153285405e8 seconds
	arrival date: 2035-12-26T17:24:37.662
	thrust profile: [-0.17155197556204754 -0.12803647772004534 -0.0010987042854903337; -0.0035589134881411667 -0.06490801713537507 0.0007426295065205218; 0.25580929199297914 -0.3791453683925915 0.015541598652070847; 0.9999998062826643 -0.5828839766311769 0.041611387112901736; 0.9999998812648976 -0.13591929443541234 0.04367451973443414; 0.9999999269970672 0.45531454218125245 0.04521667689652659; 0.9999999228048742 0.9999999183342614 0.04613770201743983; 0.840757310010811 0.9999999579385513 0.026030995407658575; 0.11987829006679744 1.0 -0.0008893319442928411; -0.16626331436648592 0.8682210906007626 -0.017523530916658536; -0.010554991808101162 0.026008419906682182 -0.0010654160560760403; -0.00038326527134042613 0.00042430859777888713 0.00034930741189383597; 8.526053802782655e-5 -0.0008985199777937706 0.000160878965697085; -0.0003967771857136998 0.0010341920913412306 -0.0002243904620731941; -0.001455496554504259 -3.155267804676458e-5 0.00028821667601580344; -0.0002685807673767674 0.000826989980715048 -0.0008420052914367241; -0.0007719825562061786 -0.0008609199968383217 -5.4081725930572875e-5; -0.00011547325119660988 0.00024382875164120964 -0.0003906884145274092; 0.0010448953162641168 -0.0012700408455061536 0.001398368665761554; -0.0009243989271800159 -0.0004827763788561335 -0.00016362116690873035] %

Mass Used: 896.7374359341643 kg
Launch C3: 23.313589250046537 km²/s²
||V∞_in||: 4.1947465879304335 km/s