archive/ES_0.56032895143903---------------------------

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: 2024-05-16T14:00:28.442
Launch V∞: [8.102719035581494, -5.835410973239287, 0.3011873881368503] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [5.440781117178352e-6, 5.3963026042871146e-5, -0.001065548511621904] km/s
	V∞_out: [-4.390238540417937e-5, 0.0010695531374559802, -1.2409687641223669e-5] km/s
	time of flight: 1.8706541066479704e8 seconds
	arrival date: 2030-04-20T16:37:18.442
	thrust profile: [0.08092395818104162 -0.000292923292609924 -0.0286675851315478; 0.07742738159230124 0.04258373238564331 -0.08816443518069403; 0.04736931034341432 0.04028839819256975 -0.09798096455357626; 0.022863390520473117 0.024867533700738246 -0.07138200488687779; 0.018039383319022644 0.023278127965873596 -0.07450920021171442; 0.021633560842027746 0.03289808848178339 -0.11386094439307902; 0.019940232337110265 0.03495595712128842 -0.1251569354949235; 0.008453267489506026 0.015181067723105898 -0.06125239754965482; 0.00680284486379065 0.012963678007671049 -0.05592403844004439; 0.00046738771922514525 0.001091303637598407 -0.005953021426565956; -0.00014325612841146958 -0.0005266315111787463 -0.0005582759788089319; 3.5536674159596115e-5 -0.00011740845655378761 0.00019004016046931561; -0.005988471140339478 0.004040969600309437 -0.007571171162693827; -0.007497602736142212 0.0035298215517888362 -0.019824027262981447; 0.002336338950150325 -0.003319860675938326 -0.00669393620493808; 0.006087217450633799 0.01517430721803128 -0.017030831827917127; 0.0052910406967254155 0.007621841832480988 -0.015261867195401289; -0.0006707861512216344 0.001834033021805938 -0.0003032160351428713; 0.0035175121923105524 -0.0007649180478209645 -0.005830562252700781; 0.0016013953249399424 -0.001496164575397235 -0.003844632600876087] %

Mass Used: 71.56916345166655 kg
Launch C3: 99.79679083894888 km²/s²
||V∞_in||: 0.0010669279455045328 km/s