archive/ES_0.5612773561160955---------------------------

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: 2024-05-12T17:59:09.796
Launch V∞: [7.906275705932641, -5.707203787874224, 0.20669274961335057] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [7.136118777224617e-7, -6.251331566369675e-6, 1.1314765267085946e-6] km/s
	V∞_out: [-9.725380791614176e-7, 3.788683389325875e-6, 5.05684748788803e-6] km/s
	time of flight: 1.8349880560966197e8 seconds
	arrival date: 2030-03-06T13:52:34.796
	thrust profile: [0.39741404988240053 -0.036845058231917464 -0.1286227621157885; 0.19992055976865508 0.07021629201526511 -0.20574861001333467; 0.04999159918186401 0.035688398744709166 -0.11172754227141407; 0.024713902084756992 0.022667156955859257 -0.08170611716315583; 0.015509335946637264 0.016612309016350257 -0.06808784245816933; 0.009674414569939895 0.01126007869382885 -0.05270909320152547; 0.012459869655711253 0.014969010621991574 -0.07687981370801904; 0.009104677308890658 0.015556357723680374 -0.06659959438064458; 0.003329052821889757 0.007325394437262008 -0.04500176294218505; 0.003688603552558504 0.006815422006400143 -0.03682723152231558; -0.0018209850828941067 0.0028282957154599337 -0.004304592542627456; -0.0010355444146127146 0.0010311339035557862 -0.007198645235326026; 0.0008935539954780317 -0.008595282164465444 -0.005071621928906292; -0.0014871130182969173 -0.0015069293913622208 -0.0021633157657973768; 0.0007323071548113136 -0.001434759240646371 -0.004812859595792045; -0.0005955357320921662 -0.005236157651460153 0.005320240888195692; -0.01232377807964937 -0.0006500033849837906 5.906022747230802e-5; 0.0005240467013258311 -0.0006539230289867987 -0.006696364064178943; 0.0005910857609952368 -0.007703924495999439 -0.009260307044970141; -0.007219139920643024 -0.005658892232202479 0.0021375031752256758] %

Mass Used: 99.93304250959045 kg
Launch C3: 95.1240925072893 km²/s²
||V∞_in||: 6.392857529713067e-6 km/s