archive/ES_0.5593270305153338---------------------------

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: 2024-05-17T00:15:46.229
Launch V∞: [7.976239070784515, -5.975432022011424, 0.08015116077466519] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [-6.778588758738583e-6, -4.7807227993082975e-5, 0.0009016736106300513] km/s
	V∞_out: [3.636473660916596e-5, -0.0009027415242873094, 1.1846576611424586e-5] km/s
	time of flight: 1.83818446774511e8 seconds
	arrival date: 2030-03-14T12:56:32.229
	thrust profile: [0.18953616876878437 -0.01342856607210278 -0.07666158984544527; 0.014562326919288666 0.00574060837007554 -0.020382968206283488; 0.050554017591673744 0.03080684850757724 -0.12135891648703964; 0.03641030566870778 0.026913987236693467 -0.12511059355710408; 0.022126859452296435 0.01824412465320203 -0.09871499892054611; 0.019058892082071774 0.01692445200523869 -0.10293334076430248; 0.017787125738772877 0.016663974903649664 -0.11174409628025024; 0.014381817762580256 0.014044206615489647 -0.10339925465531041; 0.0011769148484465967 0.0010275831224518248 -0.009692019347589528; 0.0006342791022073512 0.0004887944914799855 -0.005565208622920504; 0.004211520881521221 0.0043154536970823835 -0.03956462776673075; -8.360502184652803e-5 -0.00012340281561942472 0.0008418759482576278; 9.845742547866716e-5 -0.00017008288646478905 -4.305506347067269e-5; 0.00032679514486178994 -6.826664124090506e-5 0.0008234178726947653; -0.0008920857580903994 -0.00034538923764342857 -6.915921713698461e-5; -0.00047000290725259354 -0.0003132393157400706 0.0023550396173672343; 0.00031847506833392096 -7.223356484094211e-5 0.0002792834748352669; -0.00034354432278220644 4.577461877687142e-6 0.0025050712267480836; 0.0004215381219238164 0.0011490097126293454 0.003034279711409774; -0.00012123612672427095 -0.001274978811194512 0.004396559690357971] %

Mass Used: 73.10802526127509 kg
Launch C3: 99.33260177256247 km²/s²
||V∞_in||: 0.0009029655477484044 km/s