archive/ES_0.5561938424496837---------------------------

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: 2024-05-13T22:11:45.639
Launch V∞: [8.08167560450891, -5.7227068323935475, 0.08545705794820577] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [-4.591682274959652e-6, -4.017620824949709e-6, 3.1523118538749e-6] km/s
	V∞_out: [-4.172854223149595e-6, -5.448334253686599e-6, 2.5197687711517505e-7] km/s
	time of flight: 1.8435769892530313e8 seconds
	arrival date: 2030-03-17T16:40:03.639
	thrust profile: [0.22156120247374733 -0.010787403429675869 -0.07872440322313176; 0.047633059225183 0.023338474629914095 -0.05798335212722743; 0.04677333247823071 0.03649636743711749 -0.10104865579807687; 0.042430779910364085 0.04221763647952102 -0.13342136958718329; 0.03613689543457661 0.04238450081415168 -0.14992415380171076; 0.022561579287247523 0.03020532541892673 -0.11771652515743077; 0.012059548405890857 0.01797942738514685 -0.07650761987366188; 0.004673669786334387 0.007547053795668128 -0.034988495468994366; 0.004254127253875417 0.007516193686084113 -0.03844846249368848; 0.0005757440359198045 0.0011147327633809904 -0.006162805425979033; 0.0012997943349540523 0.002148424312998176 -0.0108301417128356; -0.0005051984627676864 -6.906149533262342e-5 -0.0009377697039247837; 0.0002573174717377667 -6.046325672607884e-5 -0.000876407044013612; -0.0007100491411729331 -0.0003698258071045472 -0.0009755556960248295; -0.0009167039824503323 0.001374756575503857 -0.0016443666051496688; -0.0003253637601406058 -0.0015813719132574695 -0.00014809238558500962; -0.0007652958371285692 9.519268620761584e-5 -0.00015795068391920823; 0.0007110309755948892 -0.0011078902120798696 -0.0008322409928800468; 0.0003619370628440967 0.0001028750543753845 0.00021583025097960935; -0.0007178242264271592 -0.0003489902512637355 -0.0029971611101825262] %

Mass Used: 76.81690050501447 kg
Launch C3: 98.0701569747914 km²/s²
||V∞_in||: 6.867451727630012e-6 km/s