archive/ES_0.5843941096820578---------------------------

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: 2023-05-02T16:26:18.464
Launch V∞: [5.444005578641176, -8.545103942330087, -0.518546309090332] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [-3.6726139895589134e-6, -1.1487555383053403e-6, 1.31986657763476e-6] km/s
	V∞_out: [-3.809293064840044e-6, 1.3160267240427651e-6, -5.408173064135109e-7] km/s
	time of flight: 1.5606671349237156e8 seconds
	arrival date: 2028-04-12T00:18:11.464
	thrust profile: [0.09797187015429194 -0.05996020706417293 -0.05847168136039344; 0.034737655654863635 -0.0075097252247751985 -0.05365821729611891; 0.05789351252188242 -0.008487740706079704 -0.15128301160278934; 0.06334589393812827 -0.00960886239353838 -0.22681026179041086; 0.05266228608365772 -0.009807767527540975 -0.2346885249369594; 0.03554293212065194 -0.0083162948802197 -0.1864217573209762; 0.018006300843000547 -0.005152993214355291 -0.1062005306694962; 0.01009957517113032 -0.003280577405743403 -0.06432449336600672; 0.004462351168480746 -0.0016826357948243975 -0.030101103245644398; 0.0035206279662412746 -0.0020595896641716948 -0.017527536534810515; 0.0008858746808152458 0.0002837057466277167 -0.008741607508625135; 0.0010282327736716123 -0.000582833611160552 -0.006874723982155823; 0.0020744368454911934 -0.0009875612721180632 -0.00736353616377044; -0.0009716624724322425 0.0006001708777416096 -0.00788593076361447; -0.00199607689493546 0.00010793464607512692 -0.00239749656892627; 0.0017803509374916104 0.0002357194469027775 -0.004084112414773065; 0.0004201670932178735 -0.0008101443360435891 -0.002872746818898042; -0.004994506438294771 -0.010852458158877594 -0.008825984779807434; 0.00015878784318195738 -0.0011846236380162194 0.0011316644042683845; 0.0011855823177636502 0.005729520117910154 -0.005370847464365322] %

Mass Used: 81.39794562806037 kg
Launch C3: 102.92488840017263 km²/s²
||V∞_in||: 4.0681421540856125e-6 km/s