archive/ES_0.5569941602771104---------------------------

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: 2024-05-13T08:16:24.907
Launch V∞: [8.055465083126876, -5.62197359649785, 0.135453538169315] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [-3.619217493740487e-9, -7.000208840015935e-9, -2.1575535886404024e-9] km/s
	V∞_out: [-7.294061326861378e-10, -1.3626087260131597e-9, -3.849767632556943e-11] km/s
	time of flight: 1.8674208000544104e8 seconds
	arrival date: 2030-04-13T17:04:24.907
	thrust profile: [0.3446927825386957 0.0012671427481388779 -0.10500762258040744; 0.04868166309195818 0.027953075223538373 -0.05532435535911624; 0.05237002102489422 0.048997630337188215 -0.10651564207136982; 0.04024656247266472 0.04988887535231583 -0.12171777194472536; 0.031585079857106846 0.04827582982073993 -0.12961498214105757; 0.01600033216465185 0.0284170582134513 -0.08524850665308843; 0.017434640634322072 0.03654817531289654 -0.11747572102875335; 0.0059801759761963025 0.01371034389784038 -0.04781746007949104; 0.00221516129261824 0.005704897514508033 -0.02138783070386524; 0.0005061110854881918 0.0006855314195764032 -0.0033278958865994353; 5.391797918452742e-5 -0.00015353371279401784 -0.00018052635183944796; -0.0006681780044537156 -0.0009987366331633584 -0.001013742278507109; -0.00022585541338218193 0.0016851826529539137 -0.003234488128161462; 0.0008251527792053232 -0.0002609045082405021 0.001048364464405695; 0.0007057820924776784 -1.3942812113515023e-5 0.00023363424319004138; 0.00024085858845254992 0.0010348768963013672 -0.001235994752877914; -0.00016849828308056715 0.0004105703661339521 0.0031131187229443843; 0.002264903535038502 0.0050752863505667675 -0.004948820592159545; 0.0026256586593523517 -0.0015421848660407663 0.00252608688289373; -0.0008466047170064802 0.00135169489371879 0.005279947001739227] %

Mass Used: 86.81971415380804 kg
Launch C3: 96.51545248619783 km²/s²
||V∞_in||: 8.170477131642283e-9 km/s