archive/ES_0.5821824918290721---------------------------

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: 2024-05-02T23:28:46.908
Launch V∞: [7.304400515338396, -5.652381733089946, 0.43275071747343946] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [-9.996794005286533e-6, 2.5524051438657195e-5, 7.459161488671935e-5] km/s
	V∞_out: [7.275127272713663e-5, 8.776162524881921e-6, -3.0506278949305744e-5] km/s
	time of flight: 1.8749577787459177e8 seconds
	arrival date: 2030-04-12T01:38:23.908
	thrust profile: [0.9450502037234153 0.022754807280144916 -0.11319658299144751; 0.44127772628285716 0.3257041137850896 -0.20604117136267253; 0.24151140513579838 0.31060861442302035 -0.21828823839909553; 0.07092117752719974 0.13120841081728254 -0.10957894417073454; 0.014328428972912567 0.0368065904216341 -0.036681604702608936; 0.004612329032117966 0.017667616544238762 -0.01915301407907797; 0.016837383343746348 0.07423874442536837 -0.07777801599562773; 0.0008148516334016581 0.003058249569863928 -0.003510266828942236; 0.0018702013472948842 0.019386801773263698 -0.023009922813310265; 0.0002447519398790057 0.0006357892798259483 -0.0015391696005496941; -7.867931986757681e-5 0.00035151188477462844 -0.0012442201197188898; -8.543633541620746e-5 0.0012476783452803556 -2.2460234113254145e-5; 0.00015245377250015758 0.0013840160047107657 -0.001880520032248617; -0.0006785229020414719 0.0002959903865572139 -0.00018702553940323302; -0.00125989481526218 -0.00042036853735002186 -0.000798534384019585; -5.837288169661234e-5 4.942374974123545e-5 0.0011803875756376866; 0.0004800872996002698 0.000588206762014463 -0.00047594207534283996; 0.0021425585570690716 0.0011756530248026326 0.00024359503152116625; -0.0020516516646443203 -0.0006498954344416237 0.0026656879323374116; 0.003369973027009908 -0.0007707688556649825 -0.001939881227176667] %

Mass Used: 180.5156443842261 kg
Launch C3: 85.49095932851851 km²/s²
||V∞_in||: 7.946900089743171e-5 km/s