archive/ES_0.5584545064603089---------------------------

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: 2024-05-10T19:25:15.707
Launch V∞: [7.952580717802071, -5.569033886875723, 0.40738539603143387] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [-2.477361872616778e-5, -0.00018362048120575589, 0.0036633806371636915] km/s
	V∞_out: [0.00015440699685011601, -0.003785111559870747, 4.8375832709257807e-5] km/s
	time of flight: 1.8607515542048427e8 seconds
	arrival date: 2030-04-03T10:57:50.707
	thrust profile: [0.4454658230972617 0.0050830570392305895 -0.12103115615158908; 0.1708675417972246 0.10566375651357973 -0.16538743111372467; 0.08101044557514815 0.08081822465293254 -0.14839106204053368; 0.03718495151878612 0.04984152409539852 -0.10358402118287627; 0.021850992651583318 0.036691262131606554 -0.084343675965843; 0.01581499034680424 0.03194976168690746 -0.08011532281250225; 0.00710512745762213 0.018489987771909563 -0.04894946178808192; 0.005594213257641363 0.015061407591417829 -0.044526199222177563; 0.0016326631280351705 0.005536203676697457 -0.016303159684928185; 0.0010260471103630837 0.003805240536911574 -0.012300142239488119; -4.8883329482639955e-6 0.00014191994665752825 -0.0003571859475706129; -0.00018249007775540075 0.0021245455194595798 -0.008904131368924404; -0.0002012911869394499 9.275617327094782e-5 -0.0008106366693252129; -0.0004809428080788795 0.0006098310839944965 -0.0006642899096192039; -0.00031329377647931907 0.0006510707133649297 0.0002527049460610165; -2.8114032560030744e-5 -0.00012473605084277608 0.0003433249146360774; 8.06379356126148e-5 0.00018083783995106691 0.0005775210158191788; 0.0008046960906766635 0.00045417270927295035 -7.303267982434276e-5; 3.4821359682178834e-5 -0.0008760086444090794 0.0012848997621455495; 0.0004694228566971653 -0.00046468127044786115 0.0009651296730446655] %

Mass Used: 100.7256828948689 kg
Launch C3: 94.42364136722712 km²/s²
||V∞_in||: 0.003668063236375414 km/s