archive/ES_0.5587996819490205---------------------------

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: 2024-05-13T08:17:22.428
Launch V∞: [7.675485625105917, -5.996728960411707, 0.5330313911610433] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [-5.801120621757737e-10, 1.498319505990795e-9, -1.7953346743542057e-9] km/s
	V∞_out: [1.1504521808211898e-9, 2.1760887200949613e-9, 5.343273735282061e-11] km/s
	time of flight: 1.832280998891993e8 seconds
	arrival date: 2030-03-04T00:59:01.428
	thrust profile: [0.3946020460568218 0.008155785284189938 -0.0928452521240498; 0.10600038783306132 0.06950961058390584 -0.09657983932412928; 0.06826086008686072 0.07588376106099566 -0.11486778823996376; 0.04239340243703908 0.06443716713488684 -0.10972379320962411; 0.03546399768122596 0.07207794857890328 -0.12894148721653675; 0.019976725228771006 0.04782978277923481 -0.09827681951445844; 0.009996756391881507 0.03527749281709128 -0.07616535480153473; 0.006237284207016486 0.018882447709266423 -0.04350332124639369; 0.004681565697763073 0.01755088606770228 -0.04245230369667058; 0.0020799505905321866 0.007492411730993483 -0.018886923431186284; 0.00043691164169171236 0.0027119896399952427 -0.007389812060644166; 3.1436852839036115e-5 0.00012840539410025235 -0.0002641861504486227; -0.00013358198580733967 -1.5702749430150973e-5 -0.0006959364008216948; -2.9191251422197703e-5 0.00017200684474477797 -0.00030732041666844934; -0.00016065136918184963 5.589635808035158e-5 -0.0001688168497299528; -2.834856940028607e-5 -0.00012508842318821129 -0.00024260709210215733; 0.0005237911619869318 0.0006259216595918761 -0.0014203223398140032; 8.314344703005746e-5 0.0003420960335515314 -0.00011491445460767329; 0.00018641543721833066 0.00029407019812886104 -0.0008281452840809888; -7.104823084563077e-5 -3.2627995137953023e-5 8.783130194768454e-5] %

Mass Used: 96.8448606999591 kg
Launch C3: 95.15796026981111 km²/s²
||V∞_in||: 2.4092982255530035e-9 km/s