archive/ES_0.5628007891454023---------------------------

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: 2024-05-10T03:10:57.207
Launch V∞: [7.743243644444229, -5.499121042273045, 0.2660228882308396] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [-8.172310953688274e-10, 1.290799913999047e-9, -1.6505528357832106e-9] km/s
	V∞_out: [1.0766881685484106e-9, 2.2047623546135412e-9, 6.106459081457821e-11] km/s
	time of flight: 1.874957778739499e8 seconds
	arrival date: 2030-04-19T05:20:34.207
	thrust profile: [0.8802032022121634 0.012150433524692137 -0.21092082212892932; 0.07851977572683698 0.0526854334365846 -0.07651349417195745; 0.0573082782745446 0.0640644871442533 -0.10216824988815407; 0.03254259955454274 0.05053320326763583 -0.09017519807706074; 0.026907234798051956 0.053538694456761265 -0.10372662741071963; 0.013112200370473625 0.03282324054196896 -0.06977061413074348; 0.005279185708603677 0.016433523425526765 -0.03828221743078651; 0.0023793893020969304 0.009694731257163382 -0.024265643936249876; 0.00567417585194894 0.025459216399734908 -0.062060552638963415; 0.0037105390516871746 0.020384359925530733 -0.05275035247936931; 0.0017817937676117101 0.011997946287791272 -0.032814202600484496; -0.000185135160681886 0.0023126105486683634 -0.00997638248595946; 0.00077018363323418 0.00031228586719202753 -0.0017150030499542258; 0.0013935488631194439 0.003889582342527941 -0.002510444500646106; -0.0012525212679856154 -0.001177384036980212 0.001137699884457924; 0.0029609110686602902 -0.0031545561382118103 0.0015738395841814131; -0.002133871719025196 0.004678869060451533 0.0064795675795594745; 0.0006616331649346011 -0.001659917105631735 0.006910926589669516; 0.0005720425802284861 -0.001704887805054019 0.006111962265635977; -0.0003772824766783353 0.0017881474659341612 0.0014147404674358498] %

Mass Used: 130.03220578379296 kg
Launch C3: 90.26892255185881 km²/s²
||V∞_in||: 2.249078865875912e-9 km/s