archive/ES_0.6145201066831925---------------------------

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: 2023-04-23T14:42:29.992
Launch V∞: [5.304670799986197, -8.65157683763653, -1.7007051899455505] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [-0.013281858048009267, 0.012660357283267476, -0.0002433538265677906] km/s
	V∞_out: [-0.005628202916512181, 7.38043568832248e-5, 0.017474015876214728] km/s
	time of flight: 1.1624159282093708e8 seconds
	arrival date: 2026-12-29T00:02:21.992
	thrust profile: [0.4119110269329402 -0.3027318628950225 -0.24255403873798095; 0.25078151322430375 -0.04740852883568603 -0.27356598718392994; 0.13231956043041543 0.0018577658493511037 -0.21381848623291427; 0.11490678007088424 0.015129629905673648 -0.23591035215921458; 0.06119188887091948 0.012271370254497373 -0.1537078405795853; 0.058237921395587075 0.013734240870169058 -0.16742781152819342; 0.06793041824938803 0.020029871727787873 -0.21163715667090974; 0.006758253882078983 0.0021283985977374694 -0.023910205126894506; 0.004551776973309636 6.408613643479183e-5 -0.008467797599320401; 0.0023882154788791607 0.0024473527676910738 -0.006442424278538805; 0.002522712621411576 -0.00034134348908153235 -0.005479257616980981; 0.0016060534763518352 -0.00180971725431532 -0.008813669923592208; -0.00024215361664483345 -0.0024863857153623412 -0.008667219740183906; -0.0015196862525379512 -0.0012463768314298043 0.004748522716620872; -0.0007754808129560441 6.585224731481379e-5 0.006989791507134144; 0.0009605115788089099 -0.0015238555231044347 0.0023704110044715787; -0.000888749054568907 -0.002820471359984391 0.0033460263888259317; -0.006794045902177847 0.0038000615897875157 -0.0037712835212130986; 0.005000512884485272 0.0026710229119683757 -0.005560286911936275; -0.007790660380066714 0.012136176059027573 0.016484779382880635] %

Mass Used: 99.29680319869158 kg
Launch C3: 105.88171221686281 km²/s²
||V∞_in||: 0.018350793466015508 km/s