archive/ES_0.6256263402653749---------------------------

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: 2024-04-24T14:45:54.668
Launch V∞: [7.530245082877718, -5.558403612276382, -0.2506990234241297] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [8.21192542412494e-6, -0.0001837009458752626, -3.4168345822806584e-6] km/s
	V∞_out: [-0.0001775222563204087, 2.7296723879600207e-5, -3.9972448099307764e-5] km/s
	time of flight: 1.874957777990453e8 seconds
	arrival date: 2030-04-03T16:55:31.668
	thrust profile: [0.9405168685690515 -0.0418051445405901 -0.11063533292341934; 0.6265502595287845 0.43149284649980885 -0.2549057293388314; 0.3208004732912881 0.39623436398012796 -0.24669239951465408; 0.15069185398231275 0.2702248988273789 -0.18492702947179593; 0.044485383396907684 0.10844015318224302 -0.08135302602077497; 0.005003610586458172 0.02749275693713115 -0.021790618697572164; 0.001777185942578947 0.010969398712163396 -0.010322066691563967; 0.0005375514483492882 0.00545313916754604 -0.00585686537919976; 3.730250128903951e-5 0.006370113096356143 -0.007246470914826857; 0.0016272679015168598 0.003475561100166138 -0.003207816021021002; 0.0003565955426401238 0.004391720483134491 -0.00561484714991707; -0.0007143518020042061 0.0035376222763304184 -0.003758874224473266; -0.0004170670200985379 0.0031173722117154162 -0.00025615308138085893; 0.0007410212063265965 0.0002562551892557409 -0.0003568533707296976; -0.00015344345543853312 0.0012876282590251848 -0.0030705528771220797; -0.00014864012231885338 0.001210956450704714 -0.00443963918993759; -4.03777519730413e-5 -0.0006106712931865383 -0.00019512003452212053; 0.0030577651894627546 0.0017511263406440095 0.00022048376896914687; -0.003999996145382249 -0.001083718175486333 0.0012128936123538942; -0.0006815153724543375 0.0003347330936975914 -0.0009280584858585518] %

Mass Used: 218.52819524408824 kg
Launch C3: 87.663291725517 km²/s²
||V∞_in||: 0.00018391614391673238 km/s