archive/ES_0.5674210681830266---------------------------

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: 2023-04-28T00:08:19.267
Launch V∞: [6.177658850487563, -7.691748936710406, -0.012684715261072189] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [3.826532278173076e-7, -2.0536436428027683e-7, -3.4587983684083697e-7] km/s
	V∞_out: [2.380096148250397e-7, -3.4688002455698586e-7, 3.6242691767952274e-7] km/s
	time of flight: 1.715554423718456e8 seconds
	arrival date: 2028-10-03T14:25:41.267
	thrust profile: [0.26887534504531285 -0.10166043529588437 -0.10595967421089819; 0.06543508386013354 0.005442730250510034 -0.07768753135502418; 0.06792249476648327 0.020115445419369302 -0.13565092975799542; 0.05309742651646169 0.022255755113982787 -0.14703558883502355; 0.04086509752709453 0.02080853014998437 -0.1437508791073373; 0.03062381790517573 0.017672242288419602 -0.1289246480909631; 0.019508310221965048 0.012717704539466624 -0.09630085971944778; 0.017219862712206224 0.012032144694847566 -0.09394919018134533; 0.008776029589451083 0.0064800976212056926 -0.05307459385872321; 0.005293126143316628 0.003974408823191037 -0.03514874028245491; 0.004806053543716352 0.003437879950514797 -0.03217543405578916; 0.003070146530073425 0.0023079660456618543 -0.0224144449405468; 0.0004303696480633727 0.0008577853390567861 -0.005852879253494182; -0.0025943594569444233 -0.0004190124198272657 -0.0031422164899725944; 0.001253019892182885 -0.0014953138697481466 -0.003540609453721752; -0.001789072838735575 -0.0031501012111925498 -0.003930274651118478; 0.003051293060271025 -0.0004780671690793098 -0.004749704498450867; -0.00045626756780864385 0.0016922939173225613 -0.002877520681154904; -0.0006037805460022104 0.0008517466304651413 -0.000619212253031326; -0.0018393566870415073 -0.005391168346684802 -0.0006694558232522641] %

Mass Used: 94.25256257789806 kg
Launch C3: 97.32663148039423 km²/s²
||V∞_in||: 5.551854432604394e-7 km/s