archive/ES_0.567073716129383---------------------------

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: 2023-05-01T04:02:52.870
Launch V∞: [6.184537126260828, -7.633084953694224, 0.2729245195187147] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [0.027258862301052608, -0.012808252464003444, 0.031881413415615956] km/s
	V∞_out: [-0.021525962241108792, -0.012748359139877532, -0.036019812043859456] km/s
	time of flight: 1.800318956450553e8 seconds
	arrival date: 2029-01-12T20:54:27.870
	thrust profile: [0.3413280822306814 -0.10854556901850454 -0.11454887538766294; 0.06254785709880986 0.012371524714775931 -0.07197045139935135; 0.05258757959215176 0.021471694525753003 -0.10064060108159656; 0.05254189285700088 0.03017767367465968 -0.13834795757318383; 0.041201013926244597 0.02936657019468059 -0.13890110508762382; 0.024665916647319343 0.019473575454441873 -0.10160315581355962; 0.02020407751135024 0.015235759403064758 -0.09079033057145384; 0.02263129203592502 0.02118187168868042 -0.11948838843576902; 0.006046213074169715 0.005268643860834736 -0.033045650337730895; 0.004569310479553515 0.005821580653932855 -0.03015409085553721; 0.003988436606793922 0.004223236644409103 -0.0268951725894898; -0.0022556089286554885 0.0020044291987744347 -0.0048585359936272636; -0.003617513653957021 -0.005942924700853594 -0.004878265958995903; -0.006428895932270643 -0.00029969915492103266 -0.005675341093916684; -0.008149385944956525 -0.0013298453412605802 0.002079541925198174; 8.116957775458665e-5 0.0031109623373466013 -0.0061464458742568045; 0.0004388739979825926 -0.0016875874295628514 1.4646175819510963e-5; 0.0036038784316582096 -0.0016855511393359854 -0.0026378506160645732; 0.0012761218441174988 -0.0076209458313890475 -0.005197739199693189; 0.008549167126592514 0.0002059015761727356 0.008480781118492193] %

Mass Used: 98.16199199397715 kg
Launch C3: 96.58697316976622 km²/s²
||V∞_in||: 0.043857968791393136 km/s