archive/ES_0.565345519821593---------------------------

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: 2024-05-08T17:46:20.194
Launch V∞: [7.8386011592321445, -5.478270788688764, 0.2845121463717499] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [1.555939334178074e-6, -8.858924373787059e-5, -1.528190068843021e-6] km/s
	V∞_out: [-8.674837443395059e-5, 1.2961187724818754e-5, -1.8951145289719446e-5] km/s
	time of flight: 1.8496974246238098e8 seconds
	arrival date: 2030-03-19T14:15:22.194
	thrust profile: [0.8047687180508053 -0.008049667367060885 -0.19303024322122986; 0.08375497918690683 0.05200650534544874 -0.08057430219691086; 0.05146914459327079 0.053967212255010284 -0.09127434083191678; 0.04392334184195442 0.06202665987263236 -0.11579711769798136; 0.0330312197961651 0.0593629590806835 -0.12063313650049796; 0.021447112402417003 0.04647945433330354 -0.10468455547241695; 0.003272333685793283 0.009629986786409011 -0.023965644605721682; 0.004392262315024267 0.014604396069871375 -0.037203438083651307; -0.0003601925574087437 0.004776007245584439 -0.013852506109321632; 0.0038022865152116635 0.01825269563060473 -0.04911770348154885; -0.0007964392752056694 0.0063699489623815185 -0.018031332127026102; 0.001197418254157728 0.007360245951986027 -0.024123684859055926; -0.0006821735593985682 0.0013137063353119021 -0.001068957431656149; -0.0022602211632518775 -9.664508918668562e-5 -0.008158848042246536; -0.008750499216382523 -0.0029085138561665753 0.0003652928447047312; 0.006369854808771891 0.0006310126792662017 0.0008310726169184221; 0.000992363071686222 -0.0031233094680592046 0.004037728690304658; -0.000609228089606247 0.008769583472503867 -0.013575885351179689; 0.004285308452127905 0.009021277885251602 -0.0038040838611153203; -0.0006669546197076481 -0.003168814223028276 3.3639772205990796e-5] %

Mass Used: 125.60938737182141 kg
Launch C3: 91.5360661291492 km²/s²
||V∞_in||: 8.861608442120423e-5 km/s