archive/ES_0.5630015779388317---------------------------

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: 2024-05-08T03:13:14.950
Launch V∞: [7.656002270286995, -5.698021576003701, 0.47798775157399476] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [6.602382760273638e-7, -2.099215343625588e-6, -6.040852698432591e-6] km/s
	V∞_out: [-5.858807437906627e-6, -6.566823427041859e-7, 2.547261968332326e-6] km/s
	time of flight: 1.84037941966225e8 seconds
	arrival date: 2030-03-08T04:52:15.950
	thrust profile: [0.5919623084155815 0.004429971568297969 -0.11809292783634341; 0.3123184664460003 0.20498018738359383 -0.21520704270713892; 0.06757944422267684 0.07711639712526813 -0.09860266304997072; 0.05731996803428009 0.09059172128193607 -0.1267138710760927; 0.04415421124026229 0.09097844062017325 -0.1359454831644557; 0.011611464969049428 0.030546693967768337 -0.05156338959171289; 0.005725260124292214 0.018332091209801393 -0.033552409950986455; 0.002314773061528126 0.008999869570366347 -0.017723953642186496; 0.004334708247758155 0.02063858902085853 -0.04020666318212626; 0.0007384485852529589 0.003504782078872773 -0.00761523931293315; 0.0003927809773925565 0.003003140882816121 -0.006697528976840447; 4.9124077317369805e-5 2.786244420111114e-6 -0.00013829808445317088; -1.167395688072e-5 4.238864955946099e-5 -0.00010645602021047744; -2.370284906339581e-5 0.00010909200216345169 -0.00015848334617547924; -2.928943943089785e-5 2.6867201527567067e-5 -0.00016108406157872593; -5.765733817916304e-5 -0.00016042094140092747 -3.1036231549279065e-5; 5.567601196958537e-5 8.689093987029776e-5 -1.612296611986898e-5; -0.00016615042097876034 -0.00015479007471122402 3.2940245252236034e-5; 4.292935907012431e-6 -6.088681994569122e-5 0.0001253288070524198; 3.7165635631059195e-5 -9.790237608518663e-5 -3.469999036492959e-5] %

Mass Used: 124.19179881423133 kg
Launch C3: 91.3102929338981 km²/s²
||V∞_in||: 6.429192870353556e-6 km/s